Method of chilling inlet air for gas turbines

ABSTRACT

A method for cooling inlet air to a gas turbine is provided. For example, a method is described including passing inlet air through a cooling coil that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant. The gas turbine power plant may include at least one gas turbine, and at least one gas turbine inlet which receives the inlet air. The method may further include passing circulating water through a water chiller at a first flow rate to reduce the temperature of the circulating water, the water chiller including a conduit through which the circulating water is capable of passing and passing the circulating water having the first flow rate through the cooling coil in an amount sufficient to lower the temperature of the inlet air. Additionally, the method may include reducing the flow rate of the circulating water passing through the water chiller, passing the circulating water through a water chiller at a second flow rate to reduce the temperature of the circulating water, the second flow rate being lower than the first flow rate, and passing the circulating water having the second flow rate through the cooling coil in an amount sufficient to lower the temperature of the inlet air.A system for cooling inlet air to a gas turbine is provided. In order to maintain a desired level of efficiency for a gas turbine plant, water is passed through a chiller to lower the water temperature. The cooled water is then circulated through coils disposed in the inlet air of the gas turbine, thereby cooling the inlet air to the gas turbine. The system may include a thermal energy storage tank for storing chilled water prior to circulation through the coils. The system may also utilize an air temperature set point selected to achieve a desired output or to meet load requirement for the gas turbine plant. The temperature or flow rate of the cooled water may be adjusted to achieve the selected air temperature set point.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No.10/206,856, filed Jul. 26, 2002, now U.S. Pat. No. 6,769,528 6,769,258which is a continuation-in-part of U.S. patent application Ser. No.09/961,711, filed Sep. 24, 2001, now U.S. Pat. No. 6,470,686, which is acontinuation of U.S. patent application Ser. No. 09/369,788, filed Aug.6, 1999, now U.S. Pat. No. 6,318,065.

BACKGROUND OF INVENTION

1. Field of the Invention

This invention relates broadly to cooling inlet air to a gas turbine.

2. Description of Related Art.

A conventional gas turbine system includes: an air compressor forcompressing the turbine inlet air; a combustion chamber for mixing thecompressed air with fuel and combusting the mixture, thereby producing acombustion gas; and a power turbine that is driven by the combustiongas, thereby producing an exhaust gas and useful power.

Over the years, various technologies have been employed to increase theamount of useful power that the power turbine is able to produce. Oneway of increasing the power output of a gas turbine is to cool theturbine inlet air prior to compressing it in the compressor. Coolingcauses the air to have a higher density, thereby creating a higher massflow rate through the turbine. The higher the mass flow rate through theturbine, the more power the turbine produces. Cooling the turbine inletair temperature also increases the turbine's efficiency.

Various systems have been devised for chilling the inlet air to thecompressor. One such system uses evaporative cooling, wherein ambienttemperature water is run over plates or over a cellular media inside ofa chamber, thereby creating thin films of water on each plate, or on themedia. The turbine inlet air is then drawn through the chamber, andthrough evaporative cooling, the air is cooled to near the wet bulbtemperature. This system is limited to cooling the air to the wet bulbtemperature, which is dependent upon the atmospheric conditions at anygiven time. Another system uses a chiller to chill water that is thenrun through a coil. The inlet air is then drawn through the coil to coolthe air. This system requires parasitic power or steam to drive thechilling system which has the further drawback that when inlet aircooling is needed the most, i.e. during the day when the temperature isthe highest, is also the time when power demand from the turbine is thehighest, i.e. during the day when power users are in operation. In orderto run the chiller, power from the turbine is required, but this poweris needed by the users of the turbines power. On the other hand, whencooling is needed the least, i.e. at night when the temperatures are thelowest, surplus power from the turbine is available because theconsumers of the turbine's power are largely not in operation.Accordingly, a continuing need exists for a turbine inlet air coolingsystem which: would efficiently cool turbine inlet air; would takeadvantage of surplus power available during times of low consumer powerdemand; and would not drain the system of power during times of highconsumer power demand.

SUMMARY OF INVENTION

A. Inlet Air Cooling

Described in greater detail below is a method for chilling inlet air toa gas turbine power plant, which may include: providing a system ofcirculating chilling water including a chilling system; providing aninlet air chiller for lowering the temperature of the inlet air beingfed to a gas turbine compressor through heat transfer between thecirculating chilling water and the inlet air, providing a thermal waterstorage tank which is operably connected to the system of circulatingchilling water, the thermal water storage tank containing chilling waterhaving a bottom; during a charge cycle, removing a first portion ofchilling water from the thermal water storage tank, passing the removedfirst portion of water through the chilling system to lower thetemperature of the removed first portion of water and to provide achilled removed first portion of water, and then introducing the chilledremoved first portion of water into the thermal water storage tank at apoint proximate the bottom of the tank, wherein the chilled removedfirst portion of water is introduced to the tank in an amount sufficientto lower the average temperature of the chilling water in the thermalwater storage tank; and during a discharge cycle, chilling the inlet airby removing a second portion of chilling water from the thermal waterstorage tank, from a point proximate the bottom of the tank and thenpassing the second portion of chilling water to the inlet air chiller tomake heat transfer contact between the second portion of chilling waterand the inlet air, such that the temperature of the inlet air islowered.

In another method that is described herein, the average temperature ofthe chilling water in the tank may be lowered to about 33° F. to about40° F. during the charge cycle and may be raised to about 60° F. toabout 70° F. during the discharge cycle. In another specific embodiment,the times of the charge and discharge cycles may be such that, beforethe temperature of the chilling water proximate the bottom of the tankreaches about 36° F. during the discharge cycle, the charge cycle isinitiated. In another specific embodiment of the method for chillinginlet air, the first portion of chilling water removed from the thermalwater storage tank during the charge cycle may be removed through a topoutlet. In yet another specific embodiment, the chilling water in thetank may have an average temperature that can be lowered during thecharge cycle and raised during the discharge cycle. In a furtherspecific embodiment of the claimed method, the discharge cycle may becarried out during the night-time and the charge cycle may be carriedout during the day-time. In still another specific embodiment, the waterlevel in the tank may remain substantially constant during the chargeand discharge cycles. In still a further specific embodiment, the one ormore chillers may be deactivated during the discharge cycle. In anotherspecific embodiment, the discharge cycle may occur during peak powerusage of the gas turbine power plant. In another specific embodiment,the discharge cycle may be performed after the removing of at least aportion of the volume of chilling water from the thermal water storagetank during the charge cycle, such that the chilled removed water thatis introduced into the thermal water storage tank at a point proximatethe bottom of the tank may remain substantially at the point proximatethe bottom of the tank. In another specific embodiment, the firstportion of chilling water removed during the charge cycle may besufficient to chill substantially all of the water in the thermal waterstorage tank to a temperature below the temperature of maximum waterdensity. In yet another specific embodiment of the claimed method, thesecond portion of chilling water removed during the discharge cycle maybe substantially all of the chilling water in the tank. In a furtherspecific embodiment of the method of the present invention, the thermalwater storage tank contains a volume of chilling water that issufficient to lower the temperature of the inlet air to a range of fromabout 45° F. to about 55° F. for a period of between about 4 hours toabout 12 hours.

Also described herein is a method of chilling water delivered to the airchiller in a gas turbine power plant system having at least one airchiller for lowering the temperature of inlet air, at least one aircompressor for compressing the inlet air, at least one combustor forburning the compressed air and providing combustion gas, and at leastone power turbine driven by the combustion gas for producing usefulpower, a method of chilling water delivered to the air chiller, themethod including the steps of: providing the at least one air chillerwith an air chiller inlet that may receive water, and an air chilleroutlet that may expel water; providing a thermal water storage tank,having a bottom portion, a top portion, at least one bottom openingproximate the bottom portion and at least one top opening proximate thetop portion, and containing a volume of stored water having an averagetemperature, and temperature of maximum water density; performing acharge cycle, by introducing through the at least one bottom opening afirst quantity of chilled water which has a chilled water temperaturethat is below the temperature of maximum water density, thereby loweringthe average temperature of the volume of stored water, wherein the firstquantity of chilled water being introduced through the bottom opening issufficient to lower the average temperature of the volume of storedwater to a temperature that is below the temperature of maximum waterdensity; and performing a discharge cycle by removing a second quantityof chilled water from the tank through the at least one bottom openingand passing the second quantity of chilled water to the air chillerinlet, to lower the temperature of the inlet air, thereby raising thetemperature of the second quantity of chilled water and providing hightemperature water, then introducing the high temperature water to the atleast one top opening in the tank.

In yet another method of chilling water, the temperature of maximumwater density may be from about 20° F. to about 39.2° F. In anotherspecific embodiment, the temperature of maximum water density may beabout 39.2° F. In another specific embodiment, the temperature of thestored water may have a temperature of from about 34° F. to about 40° F.In yet another specific embodiment of the claimed method the temperatureof the stored water may have a temperature corresponding to the maximumwater density of about 39.2° F. In another specific embodiment sodiumnitrate may be added to depress the freezing temperature of the waterthereby allowing stored water to be in the range of about 25° F. toabout 34° F. In another specific embodiment of the method of the presentinvention, the useful power produced by the power turbine may beconsumed at a variable rate, and the charge cycle may be performed whenthe rate is at a minimum. In a further specific embodiment, the usefulpower produced by the power turbine may be consumed at a variable rate,and the discharge cycle may be performed when the rate is at a maximum.In yet another specific embodiment of the method of the presentinvention, the quantity of water expelled during the discharge cycle maybe less than the volume of stored water. In a further specificembodiment, the quantity of chilled water may be chilled by passingwater through at least one chiller. In still another specific embodimentof the claimed method, the temperature of inlet air may be lowered froma high temperature of from about 85° F. to about 95° F. to a lowtemperature of from about 45° F. to about 55° F. In still a furtherspecific embodiment, the high temperature may be about 90° F. and thelow temperature may be about 50° F. In yet another specific embodiment,the output of the gas turbine power plant system may be from about 50megawatts to about 250 megawatts.

Also described below is a gas turbine power plant system, wherein thesystem includes: one or more air chillers for lowering the temperatureof inlet air; one or more air compressors for compressing the inlet air;one or more combustors for burning the compressed air and providingcombustion gas; and one or more power turbines driven by the combustiongas for producing useful power, and an improvement that may include: athermal water storage tank for containing chilled water, wherein thethermal water storage tank has a bottom portion with a bottom outlet anda top portion, and the tank is operably connected to the air chillersuch that the chilled water passes from the bottom outlet to the airchiller to lower the temperature of the inlet air and is returned to thethermal water storage tank; and a water chilling system for chilling thewater in the thermal water storage tank, wherein the water chillingsystem is configured to receive high temperature water from the topportion of the tank, and wherein the system is configured to introducelow temperature water to the bottom portion of the tank, such that theaverage temperature of the water in the tank is lowered; and wherein thewater chilling system includes one or more chillers for lowering thetemperature of the high temperature water from the top portion of thetank to provide low temperature water.

In an example of such a gas turbine power plant system, the thermalwater storage tank may have a bottom, and the bottom outlet may bepositioned at a height that is less than about 10 feet from the bottomof the tank. In another specific embodiment of the gas turbine powerplant system, the thermal water storage tank may have a bottom, and thebottom outlet may be positioned at a height that is less than about 5feet from the bottom of the tank. In another specific embodiment, thethermal water storage tank may have a bottom, and the bottom outlet maybe positioned at a height that is less than about 18 inches from thebottom of the tank. In another specific embodiment, the tank may have atop outlet and a bottom inlet such that, in a charge cycle the hightemperature water may be removed through the top outlet and may be fedto the one or more chillers, and the low temperature water may beintroduced to the tank through the bottom inlet. In a further specificembodiment of the gas turbine power plant system, the tank may have abottom outlet such that, in a discharge cycle, chilling water may beremoved from the tank through the bottom outlet. In still a furtherspecific embodiment of the gas turbine power plant system, the tank mayhave a bottom outlet such that, in a discharge cycle, chilling water maybe removed from the tank through the bottom outlet, fed to the airchiller and is returned to the tank, bypassing the one or more chillersof the water chilling system. In still a further specific embodiment ofthe gas turbine power plant system, the top portion may be separatedfrom the bottom portion by a thermocline.

In yet another example, during the charge cycle, the bottom inlet mayreceive a quantity of chilled water that is sufficient to supply the airchiller with water having a temperature below the temperature of maximumwater density for four or more hours. In another specific embodiment,during the charge cycle, the bottom inlet may receive a quantity ofchilled water that is sufficient to supply the air chiller with waterhaving a temperature below the temperature of maximum water density foreight or more hours. In still another embodiment, during the chargecycle, the bottom inlet may receive a quantity of chilled water that issufficient to supply the air chiller with water having a temperaturebelow the temperature of maximum water density for twelve or more hours.

In still another example, the thermal water tank may have a height offrom about 25 feet to about 70 feet. In yet another specific embodiment,the thermal water tank may have a diameter of from about 50 feet toabout 250 feet. In another specific embodiment, the thermal water tankmay have a diameter, and a height, and the diameter may be greater thanthe height. In yet another specific embodiment of the claimed invention,the volume of stored water may be greater than about eight hundredthousand gallons. In still a further specific embodiment, thetemperature of the water in the top portion may be about 15° F. to about35° F. greater than the temperature of the water in the bottom portion.In another specific embodiment, the thermal water storage system mayinclude a plurality of thermal water storage tanks, each of theplurality of tanks may have a bottom inlet and a bottom outlet, and eachof the plurality of tanks may have a top inlet and a top outlet. Inanother specific embodiment, the bottom inlet may have a bottomdiffuser, and the top inlet may have a top diffuser, whereby the waterentering the bottom inlet is diffused, and the water entering the topinlet may be diffused. In yet another specific embodiment, thetemperature of the water in the top portion of the tank may have atemperature ranging from about 60° F. to about 70° F. In still a furtherspecific embodiment, the temperature of the water in the bottom portionof the tank may have a temperature that is above the freezingtemperature. In another specific embodiment, the water chilling systemmay include at least one mechanical chiller. In still another specificembodiment of the present invention, the water chilling system mayinclude at least one absorption chiller. In still a further specificembodiment, the water chilling system may include at least onemechanical chiller and at least one absorption chiller. In yet anotherspecific embodiment, the mechanical chiller may receive chilled waterfrom the absorption chiller, and the mechanical chiller may furtherchills the chilled water. In another specific embodiment, the gasturbine power plant system may additionally including a heat recoverysteam generator and a steam turbine, wherein the absorption chiller maybe driven by steam from the heat recovery steam generator. Anotherspecific embodiment of the gas turbine power plant system mayadditionally include a heat recovery steam generator and a steamturbine, wherein the absorption chiller is driven by back pressure fromthe steam turbine exhaust. In another specific embodiment, the inlet airmay be lowered from a first temperature of about from 85° F. to about95° F. to a second temperature of from about 45° F. to about 55° F. inthe inlet air chiller. In yet another embodiment, the first temperaturemay be about 90° F. and the second temperature may be about 50° F. Inanother specific embodiment of the gas turbine power plant system, thechilling water being fed to the inlet air chiller may have a temperatureof from about 34° F. to about 40° F. In another specific embodiment, thegas turbine power plant system may additionally include a steam turbineand a heat recovery steam generator, and the heat recovery steamgenerator may receive exhaust gas from the power turbine and may providehigh pressure steam to the steam turbine, and the steam turbine mayprovide low pressure steam.

B. Additional Methods and Systems

Embodiments of the invention additionally include passing inlet airthrough a cooling coil that includes an opening for receiving the inletair and that is operably connected to a gas turbine power plant. The gasturbine power plant may include at least one gas turbine, and at leastone gas turbine inlet which receives the inlet air. The method mayfurther include passing circulating water through a water chiller at afirst flow rate to reduce the temperature of the circulating water, thewater chiller including a conduit through which the circulating water iscapable of passing and passing the circulating water having the firstflow rate through the cooling coil in an amount sufficient to lower thetemperature of the inlet air. Additionally, the method may includereducing the flow rate of the circulating water passing through thewater chiller, passing the circulating water through a water chiller ata second flow rate to reduce the temperature of the circulating water,the second flow rate being lower than the first flow rate, and passingthe circulating water having the second flow rate through the coolingcoil in an amount sufficient to lower the temperature of the inlet air.

Additional embodiments may include providing a system of circulatingliquid chilling water including a chilling system that includes a firstmechanical chiller and a second mechanical chiller, the first and secondmechanical chillers being arranged in series and passing at least aportion of the liquid chilling water through the first mechanicalchiller and the second mechanical chiller, the liquid chilling waterpassing through the first mechanical chiller being lowered to a firsttemperature, and the liquid chilling water passing through the secondmechanical chiller being lowered to a second temperature that is lowerthan the first temperature, thus providing a staged liquid chillingwater temperature drop, wherein the staged liquid chilling watertemperature drop is from about 20° F. to about 34° F. The method mayfurther include providing an inlet air chiller, comprising a coolingcoil through which liquid chilling water passes, for lowering thetemperature of inlet air being fed to the compressor through heattransfer between the liquid chilling water passing through the coolingcoil and the inlet air, wherein the inlet air chiller provides a liquidchilling water temperature rise of from about 20° F. to about 34° F. andchilling the inlet air by directing the liquid chilling water to theinlet air chiller and passing the liquid chilling water through thecooling coil of the inlet air chiller to make heat transfer contactbetween the liquid chilling water and the inlet air. Preferably, themethod additionally includes adding potassium formate to the circulatingwater in an amount sufficient to depress the freezing point of thecirculating water. In the alternative, or additionally, the method mayinclude contacting the inlet air leaving the cooling coil with a controlsystem, a temperature sensor, and a relative humidity sensor to monitorthe leaving air temperature and relative humidity of the leaving air andvarying the flow or the temperature of the circulating water to maintaina relative humidity of the coil to below about 95% to about 99% RH foroptimal efficiency in a combined cycle system.

Additional embodiments may include a system for chilling inlet air for agas turbine power plant including passing inlet air through a coolingcoil that includes an opening for receiving the inlet air and that isoperably connected to a gas turbine power plant that includes at leastone gas turbine, and at least one gas turbine inlet which receives theinlet air, passing circulating water through a water chiller at a firstflow rate to reduce the temperature of the circulating water, the waterchiller including a conduit through which the circulating water iscapable of passing and passing the circulating water having the firstflow rate through the cooling coil in an amount sufficient to lower thetemperature of the inlet air to a desired air temperature setpoint. Thesystem may further include reducing the flow rate of the circulatingwater passing through the water chiller during lower ambient off-designperiods to maintain the desired air temperature setpoint, passing thereduced flowrate circulating water through the water chiller at a secondflow rate and reducing the temperature of the circulating water tomaintain the desired air temperature setpoint, the second flow ratebeing lower than the first flow rate and passing the circulating waterhaving the second flow rate through the cooling coil in an amountsufficient to lower the temperature of the inlet air to the desired airtemperature setpoint. The method may additionally include reducing theflow rate of the circulating water passing through the two or moresequentially positioned compressors during lower ambient off-designconditions to maintain a higher circulating water delta T therebyallowing warmer water to pass through the upstream compressor thusimproving the efficiency at partial load.

Certain embodiments include passing the circulating water through aheater prior to passing the circulating water through the cooling coil,in which the circulating water temperature is increased to a temperaturethat is higher than the temperature of the circulating water leaving thecooling coil and higher than the temperature of the air entering thecooling coil to maintain the minimum desired leaving air temperature.

Certain embodiments include adding an additive to the circulating waterin an amount sufficient to depress the freezing point of the circulatingwater. Certain embodiments may further include adding an additive to thecirculating water in an amount sufficient to depress the freezing pointof the circulating water and minimizing any negative performancederating due to the additive effect on the heat transfer properties ofwater. Certain embodiments may include adding a salt additive to thecirculating water in an amount sufficient to depress the freezing pointof the circulating water. The salt additive may be added to thecirculating water in an amount sufficient to depress the freezing pointof the circulating water to a point that would specifically provide forprotection of the system during low ambient temperature operation and toprotect the system during shut-down periods. Certain embodiments mayinclude adding sodium nitrate to the circulating water in an amountsufficient to depress the freezing point of the circulating water. Inyet other embodiments, the method includes adding potassium formate tothe circulating water in an amount sufficient to depress the freezingpoint of the circulating water.

In certain embodiments, the method includes determining a set point andreducing the flow rate of the circulating water passing through thewater chiller when the temperature difference between the circulatingwater entering the cooling coil and the circulating water leaving thecooling coil reaches the set point. Certain embodiments includedetermining a leaving chilled water temperature set point and increasingthe setpoint at reduced off-design ambient temperatures to maintain thedesired air temperature off the coil until the temperature differencebetween the circulating water entering the cooling coil and thecirculating water leaving the cooling coil reaches a minimum set pointand reducing the flow rate of the circulating water passing through thewater chiller and reducing the leaving chilled water temperaturesetpoint to maintain the desired air temperature off the coil.

Certain embodiments include passing the circulating water through a pumpprior to passing the circulating water through the water chiller. In yetother embodiments, the method includes passing the circulating waterthrough a pump prior to passing the circulating water through the waterchiller, reducing the circulating water flowrate, and decreasing thetemperature of the circulating water to maintain the desired leaving airtemperature. Certain embodiments include passing the circulating waterthrough one or more pumps and reducing the flow rate of the circulatingwater by shutting off at least one of the one or more pumps. Optionally,the method may include passing the circulating water through one or morepumps mounted in parallel and reducing the flow rate of the circulatingwater by shutting off at least one of the one or more pumps duringpartial load conditions. In yet other embodiments, the method includespassing the circulating water through one or more pumps and reducing theflow rate of the circulating water by lowering the speed (RPM) of thepump via a variable frequency drive on the one or more pump motors.

In certain embodiments, the gas turbine inlet air temperature leavingthe cooling coil is about 40° F. to about 60° F. Certain embodimentsinclude providing a temperature sensor contacting the inlet air leavingthe cooling coil to monitor the inlet air temperature. In yet otherembodiments, the method includes providing a temperature sensorcontacting the inlet air leaving the cooling coil to monitor the inletair temperature and lowering the temperature of the inlet circulatingwater when the inlet air temperature increases above the setpoint. Incertain other embodiments, the method includes providing a wet bulbtemperature sensor to monitor the ambient air wet bulb temperatureentering the cooling coil. In yet other embodiments, the method includesproviding a control system and a temperature sensor contacting the inletair leaving the cooling coil to monitor the inlet air temperature andlowering the circulating water flowrate when the temperature differencebetween the circulating water entering the cooling coil and thecirculating water leaving the cooling coil decreases to from about 50%to about 90% of the difference between the ambient air wet bulbtemperature entering the cooling coil and the temperature of the leavingair.

In certain embodiments, the chilled water temperature entering thecooling coil is about 34° F. to about 45° F. In certain embodiments, thecooling coil includes a multipass cooling coil. In other embodiments,the cooling coil includes a four pass cooling coil. In yet otherembodiments, the cooling coil includes a six pass cooling coil.

In certain embodiments, the water chiller includes an evaporator.Certain embodiments additionally include providing a thermal waterstorage tank which is operably connected to the water chiller. In yetother embodiments, the method includes providing a thermal water storagetank which is operably connected to the water chiller and during acharge cycle, removing a first portion of circulating water from thethermal water storage tank, passing the removed first portion of waterthrough the water chiller to lower the temperature of the removed firstportion of circulating water and to provide a chilled removed firstportion of water, and then introducing the chilled removed first portionof water into the thermal water storage tank, wherein the chilledremoved first portion of water is introduced to the tank in an amountsufficient to lower the average temperature of the circulating water inthe thermal water storage tank. Certain embodiments include providing athermal water storage tank which is operably connected to the waterchiller and during a discharge cycle, chilling the inlet air by removinga second portion of water from the thermal water storage tank and thenpassing the second portion of water to the inlet cooling coil to makeheat transfer contact between the second portion of the circulatingwater and the inlet air, such that the temperature of the inlet air islowered.

Certain embodiments include controlling the inlet air temperatures ofmultiple gas turbines by throttling the flow of circulating water to thecooling coil of the gas turbine which has the lowest turbine inlet airtemperature. In yet other embodiments, the method includes controllingthe inlet air temperatures of multiple gas turbines by throttling theflow of circulating water to the cooling coil of the gas turbine whichhas the lowest turbine inlet air temperature and resetting the supplycirculating water setpoint higher once the last gas turbine circulatingwater is throttled to maintain the desired turbine inlet air temperatureuntil at least one of the gas turbines meets the desired inlet airtemperature without throttling more than about 25% of fully open.

Additional embodiments include passing inlet air through a cooling coil,passing circulating water through a water chiller to reduce thetemperature of the circulating water and to provide chilled water,passing the chilled water through the cooling coil to lower thetemperature of the inlet air and to provide chilled inlet air andsupplying water in a fog to the chilled inlet air downstream of thecooling coil in an amount sufficient to supersaturate the alreadysaturated chilled inlet air.

Certain embodiments include removing a portion of water from the inletair via the condensate off of the cooling coil and then reintroducingthat water through a high pressure spray or fog to the chilled inletair. In yet other embodiments, the method includes providing acompressor within the gas turbine power plant, in which supplying water(fog) to the chilled inlet air includes entraining water in the chilledinlet air in an amount sufficient to lower the temperature of at leastone stage of the compressor. In certain embodiments, the method includespassing the chilled inlet air through a compressor to vaporize the waterin the chilled inlet air and cool interstages of the compressor. Incertain embodiments, the chilled inlet air is at a saturation level. Incertain embodiments, the chilled inlet air is at a supersaturation levelafter the water is supplied. The method may additionally includeremoving a portion of water from the inlet air via the condensate off ofthe cooling coil to be stored until the chilling system is off and thenreintroducing that water to be evaporated in the airstream by means of ahigh pressure spray or fog and thereby achieving evaporative cooling tonear the wetbulb temperature.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic diagram of a sequential turbine inlet air coolingsystem showing optional enhancements.

FIGS. 2A and 2B are schematic diagrams of an alternative embodiment ofthe turbine inlet air cooling system wherein the gas turbine exhaustheat is used.

FIG. 3 is a side view of a storage tank.

FIG. 4 is a schematic diagram of an alternative embodiment of a turbineinlet air cooling system showing sequential cooling of two in-seriescounterflow duplex chillers and multi-pass cooling coil.

FIG. 5 is a schematic diagram of a 6 pass cooling coil useful in veryhigh delta T thermal storage embodiments of the present invention;

FIG. 6 is a psychrometric chart showing the various operating points ofa cooling coil when operating in an optimal capacity mode or an optimalcombined cycle efficiency mode of operation.

FIG. 7 is a chart showing example data.

DETAILED DESCRIPTION

Specific embodiments of the invention will now be described. However, aperson of ordinary skill in the art will recognize that the inventionwill actually be defined by one or more of the claims, rather than thedescription below. Depending on the context, all references to the“invention” below may in some cases refer to certain specificembodiments only. In other cases it will be recognized that referencesto the “invention” will refer to subject matter recited in one or more,but not necessarily all, of the claims.

A. Inlet Air Cooling

Generally, referring to FIG. 1, the overall apparatus 10 includes aconventional gas turbine system 12 having an air chiller 14, e.g., aconventional cooling coil, for lowering the temperature of inlet air,shown schematically by arrow 15a, from ambient temperature (T1, e.g.,about 90° F. (about 32° C.), or in the range of from about 70° F. (about21° C.) to about 85° F. (about 29° C.) to a range of from about 100° F.(about 38° C.) to about 115° F. (about 47° C.)), or to about 125° F.(about 52° C.) to provide compressor feed air, shown schematically byarrow 15b, having some lower temperature (T2, e.g., about 50° F. (about10° C.), or in the range of about 45° F. (about 7° C.) to about 55° F.(about 13° C.)), or to about 60° F. (about 16° C.). The air chiller 14can be a conventional cooling coil that provides for heat transfercontact, e.g., across a set of coils within the air chiller 14, betweenthe circulating chilling water 16c (preferably at a T3 of about 34° F.(or about 1° C. to about 2° C.) to about 40° F. (or about 4° C. to about5° C.)) and the inlet air 15a, forming chilled compressor feed air 15b,and resulting in a higher temperature circulating water 16d (T4, e.g.,about 54° F. (about 12° C.) to about 60° F. (about 16° C.)). A preferredcooling coil may be specially circuited so as to achieve relatively highchanges in the temperature of the water flowing through the tubes in thecooling coil. This rise in temperature is preferably in a range of about20° F. (about 11° C.) to about 35° F. (about 19° C.) on a hot designday. As used herein a “design day” is the maximum temperature that theambient air is expected to reach—the temperature upon which the systemdesign is based. The chilled compressor feed air 15b may then beintroduced to a conventional gas turbine (GT) compressor 32, where it iscompressed, combined with fuel and burned in a conventional combustor 34to produce a combustion gas that can be used for driving the powerturbine 36, resulting in “exhaust gas.” FIG. 2A shows one embodiment ofthe overall system as including only one gas turbine system 10, one airchiller 14, one water chilling system 13, and one optional tank 18.However, depending upon system requirements as well as geographical,geological, and other constraints, it may be desirable to have more thanone gas turbine system 12, more than one air chiller 14, more than onewater chilling system 13, or more than one tank 18.

FIG. 2A shows a combined cycle system whereby exhaust from the powerturbine 36 can be passed through a heat recovery steam generator (HRSG)38 to produce steam, shown schematically by arrow 44, and “stack gas,”shown schematically by arrow 45. Further, in another embodiment of acombined cycle system, a heat recovery coil 42 may receive the exhaustgas 45 from the power turbine 36 and produce hot water or steam, shownschematically by arrow 48. The hot water or steam 48 produced either bythe HRSG 38 or the heat recovery coil 42 may advantageously be used tosupply power to an absorption chiller 26, the importance of which willbe discussed below.

As mentioned, it is advantageous to lower the temperature of the inletair 15a to a temperature T2 that is as low as possible. The change inair temperature from T1, before entering the air chiller 14, to T2,after exiting the air chiller 14, is referred to herein as ΔT. Evensmall increases in ΔT, i.e., lowering T2 can affect significantincreases in the capacity of the gas turbine system. For example, in aparticular gas turbine, an increase in ΔT of about 2.6° F. (about 1° C.to about 2° C.) may increase the turbine output by about one percent.

Included in FIG. 1 is a circulating water system or loop, which includescirculating chilling water 16 that circulates through the speciallycircuited, high ΔT air chiller 14 and back through chillers piped inseries to an optional thermal water storage tank 18 for storing thechilling water 16. The term “loop” preferably refers to conventionalpipage, e.g. pvc or steel pipes having valves (not shown) whereappropriate. The features of this chilling water loop will now bedescribed with reference to FIG. 1, where, for ease of comprehension,the water within the loop is referred to generally with numeral 16, andthe various streams of water within the loop are referred to with thenumeral 16 followed by an alphabetic character to distinguish betweenvarious streams of water where necessary.

The chilling water loop includes a water chilling system 13. The waterchilling system 13 may include any number of conventional water chillersinstalled either in parallel or in series but preferably with at leasttwo chillers piped in series so as to stage the temperature drop of thewater into an intermediate and a lower temperature chiller. This savespower on the upstream chiller and makes the system more efficient. Ifthe power plant is a combined cycle plant and if there is sufficientexhaust energy available from either the steam turbine exhaust (stream46) or heat recovery coil (stream 48), then it is preferable as shown inFIG. 2A for the water chilling system 13 to include an absorptionchiller 26 which may derive its power from the heat energy recoveredfrom the HRSG 38, or the heat recovery coil 42, or both, and amechanical chiller 24. The absorption chiller 26 and the mechanicalchiller 24 are shown in series, as that is the preferred arrangementwith the absorption chiller placed upstream of the mechanical chiller,however they may be placed in parallel depending upon system needs. Ifexcess waste heat is not available at a sufficiently low cost, theupstream chiller is preferably a mechanical chiller. An object of thewater chillers is to chill the chilling water 16 to a sufficiently lowtemperature so that the chilling water 16 can then be used to chill theinlet air 15a in the air chiller 14 with a minimum water flow rate andmaximum water ΔT. Preferably, the temperature of the chilling water 16cis about 34° F. (about 1° C. to about 2° C.) to about 40° F. (about 4°C. to about 5° C.) prior to entering the air chiller 14. A number ofconventional devices can be used to chill the water going to the waterstorage tank 18. For example, the chilling water can be chilled beforeit is ever introduced to the tank, by passing the chilling water 16dfrom the air chiller either through a mechanical chiller 24 or anabsorption chiller 26 (driven by hot water or steam 44, 48 from the HRSGor LP steam 46 coming out of the steam turbine 40) to provide chillingwater 16a that is then introduced to the tank 18. A hybrid chillingarrangement can also be used whereby both mechanical 24 and absorption26 chillers are used in combination. The preferred arrangement is tocirculate the warm water 16e from the tank 18 or the heated water 16dfrom the air chiller 14 to the upstream absorption (or mechanical)chiller 26 first where the water 16d will be chilled from range of about54° F. (about 12° C.) to about 65° F. (about 19° C.) to a range of about40° F. (or about 4° C. to about 5° C.) to about 48° F. (or about 8° C.to about 9° C.). The water 16d then circulates through the downstreammechanical chiller 24 where it may be chilled further to about 34° F.(or about 1° C. to about 2° C.) to about 40° F. (or about 4° C. to about5° C.).

The thermal water storage tank 18 is preferably a thermally insulatedvessel, having an upper opening or connection or top inlet/outlet 20. Inother specific embodiments, e.g., where an open tank is used, the top“opening” or top inlet can be the open top of the tank, so that watercan be piped into the tank through the top. The tank 18 may be made fromany material having the strength and insulation qualities necessary fora thermal water storage tank, however, preferably, the tank 18 isconstructed of steel or concrete. The top inlet/outlet 20 (also referredto herein as an “opening”) both receives heated water 16d from the airchiller 14 during a discharge cycle, and expels heated water 16e duringa charge cycle. (The charge and discharge cycles will be explained infurther detail below) The thermal water storage tank 18 preferably alsohas a lower connection or bottom inlet/outlet 22 (or “opening”). Thebottom inlet/outlet 22 both receives chilled water 16a from waterchilling system 13 during the charge cycle, and discharges chilled water16b to the air chiller 14 during the discharge cycle. Furthermore, thesystem shown in FIG. 1 also allows a “partial storage” strategy wherebythe chilled water in the tank can be used to supplement the waterproduced by the chillers such that both can be provided to the airchiller 14 to allow longer periods of on-peak chilled air going to thegas turbine.

Preferably, in the system in FIG. 2A, the water 16 in the tank 18 is“stratified” according to temperature. That is, the lower temperaturewater (about 33° F. (about 0° C. to about 1° C.) to about 40° F. (about4° C. to about 5° C.)) resides at the bottom of the tank. Broadly, thetemperature at the bottom of the tank may be in the range of from about33° F. (about 0° C. to about 1° C.) to about 40° F. (about 4° C. toabout 5° C.). Preferably, the temperature of the water in the bottom ofthe tank is in the range of from about 33° F. (about 0° C. to about 1°C.) to about 36° F. (about 2° C. to about 3° C.). Most preferably thetemperature of the water in the bottom of the tank is in the range offrom about 33° F. (about 0° C. to about 1° C.) to about 34° F. (about 1°C. to about 2° C.). The higher temperature water (typically about 60° F.(about 16° C.) to about 70° F. (about 21° C.), typically having a lowerdensity, remains at the upper portions of the tank.) Preferably, theentire tank 18 will be occupied by lower temperature water (about 33° F.(about 0° C. to about 1° C.) to about 34° F. (about 1° C. to about 2°C.)) after a charge cycle (discussed below) is completed. The tankshould be capable of storing sufficient chilled water 16 to provide aircooling during an entire discharge cycle (discussed below). Further, thetank 18 should have a sufficient height so that adequate temperaturegradients can be maintained. Preferably, the diameter of the tank 18 isgreater than the height. An advantage of using the charge/dischargecycles, and other features of the present invention is realized withrespect to the natural tendency of water to “stratify” according totemperature. Generally, in the temperature range of about 39.2° F.(about 4.0° C.) to about 212° F. (100° C.), water decreases in densityas temperature increases. As a result, the colder water sinks to thebottom and the warmer water rises to the top, thereby forming uniformtemperature strata or layers. Further, in the temperature range of about32° F. (about 0° C.) to about 39.2° F. (4.0° C.), water tends toincrease in density according to temperature. As a result, in thistemperature range, the warmer water tends to sink to the bottom and thecolder water rises to the top. Generally, pure water reaches its maximumdensity at about 39.2° F. (about 4.0° C.). However, depending uponatmospheric conditions, or if various chemicals are added to the water,the temperature of maximum water density may change. Therefore, if thecharge/discharge cycles of the claimed invention are not performed, thecoldest water does not sink to the bottom, but instead, water with atemperature of about 39.2° F. (about 4.0° C.) naturally tends to settletoward the bottom of the tank. The tank 18 of the claimed inventiondischarges warm water 16e from the top portion 18a of the tank 18, andreceives chilled water 16a from the water chilling system 13, which isbelow the temperature of maximum water density, during the charge cycleinto the bottom portion 18b through bottom inlet/outlet 22. In thismanner, the coldest but not necessarily the heaviest water is forcedinto the bottom. Further, as mentioned, the charge cycle preferably islong enough and the charge flow rate is great enough to fill the entiretank 18 with the design cold water temperature by the end of the chargecycle. Even if the tank is not chilled with water that is below thetemperature of maximum water density (i.e., below about 39.2° F.), thewater 16 in the tank 18 is preferably not allowed to remain stagnant inthe tank 18 long enough for the densest but not the coldest water tosink to the bottom of the tank 18. During the discharge cycle, water ispreferably taken from the bottom portion 18b of the tank 18 through thebottom inlet/outlet 22 thereby ensuring that the coldest water isremoved and directed to the air chiller 14. As it is preferable to havethe coldest water remain in the bottom portion 18b of the tank 18, andhave the warmest water remain in the top portion 18a of the tank 18, itis generally desirable to prevent unnecessary mixing or global movementof the water 16 in the tank 18. For this purpose, a diffuser 23a, 23b(FIG. 3) may be disposed adjacent the bottom inlet/outlet 22 and topinlet/outlet 20. Generally, the diffusers 23a, 23b tend to reduce thevelocity of the water entering or leaving the tank to minimize anyturbulent mixing.

It may also be advantageous to allow some of the chilled water to flowthrough the air chiller 14, during the charge cycle, to provide somecooling to the gas turbine. In this manner, the thermal water storagetank 18 will be charged with chilled water, and some cooling of theinlet air can also be accomplished.

Referring to FIG. 3, a preferred embodiment of the thermal water storagetank 18 will be discussed. The tank has a top 18c, a bottom 18d, and afoundation 18e. Top inlet 20b and top outlet 20a are shown as a singleport or connection to the diffuser which is adapted to accommodate abidirectional flow, i.e. either into the tank, 20b, or out of the tank,20a. However, it should be noted that top inlet 20b and top outlet 20amay also be two separate ports or orifices, one being an inlet 20b, theother being an outlet 20a. The same is true for bottom inlet 22b andbottom outlet 22a, which are shown as a single ports in FIG. 3. As shownin FIG. 3, top diffuser 23a and bottom diffuser 23b are essentially longpieces of pipe or tubing with slots cut perpendicular to their length.In operation, the slots in top diffuser 23a point toward the top 18c oftank 18, and the slots in bottom diffuser 23b point toward the bottom18d of tank 18. In this manner, when water flows into one of the inlets20b, 22b and through the corresponding diffuser 23a, 23b the flowingwater generally does not create global currents in the tank. Preferably,the diffusers 23a, 23b prevent mixing of the warmer water in the topportion 18a with the cooler water in the bottom portion 18b. Otherdiffuser designs may also be used. Some of these designs includeoctagonal diffusers which are formed by eight straight sections of pipeconnected with 45° elbows. A series of equally sized, shaped, and spacedlateral slot openings are cut into the top of the straight sections ofpipe in a manner similar to the slots cut in the diffuser shown in FIG.3. Some diffusers have circular holes rather than slots. Other types ofdiffusers include radial disk diffusers which consist of two closelyspaced disks, mounted parallel to the tank floor. In a radial diskdiffuser, the incoming water flows between the disks and enters the tankhorizontally.

Also shown in FIG. 3 is the thermocline 19, which is shown as a thinband. The thermocline 19 separates the cold water in the bottom portion18b of the tank 18 from the warmer water in the top portion 18a. Thebottom portion 18b of the tank 18 is that part of the tank 18 that isbelow the thermocline 19, and the top portion 18a of the tank 18 is thatportion of the tank 18 that is above the thermocline 19. As mentioned,the thermocline will move up and down during the charge and dischargecycles respectively. The distance from the bottom 18d of the tank 18 tothe thermocline 19 is denoted in FIG. 3 as H2. It is advantageous toposition the bottom inlet 22b and the bottom outlet 22a at a height H1that is below the thermocline 19 at its lowest point at the end of thedischarge cycle. In so doing, generally the warmer water above thethermocline 19 should not be expelled out of the bottom outlet 22a tothe air chiller 14 during the discharge cycle. In FIG. 3, the height ofthe bottom inlet 22b and the bottom outlet 22a are signified by H1, butit is to be understood that the bottom inlet 22b and the bottom outlet22a may be at the same or different heights depending upon therequirements of the specific system. Preferably H2 is maintained at aheight that is greater than H1, so that during the discharge cycle, thewarmer water in the top portion 18a will not be expelled through thebottom outlet 22b. Generally, the tank 18 is sized, according toparameters described below, so that the height H2 of the thermocline maynot fall below a height of less than about 10 feet. More preferably, thedesign tank size will be reduced such that the height H2 is less thanabout 5 feet, and most preferably, the tank size will be reduced towhere height H2 is only about 18 inches during a complete dischargecycle on a design hot day.

During the discharge cycle, the heated water 16d from the air chiller 14is introduced into the top portion 18a of the tank 18 through topinlet/outlet 20. This heated water 16d tends to remain above the chilledwater 16b. At the level where the heated water meets the chilled waterthere may be a “thermocline,” represented by line 19. A thermocline is ahorizontal region that separates higher temperature water from lowertemperature water. The bottom portion 18b of the tank 18 is below thethermocline 19 and the top portion 18a is above the thermocline. Thebottom inlet/outlet 22 may be disposed at the very bottom 18d of thetank 18. However, the bottom inlet/outlet 22 may alternatively bepositioned at any height so long as it is in the bottom portion 18b ofthe tank 18. Similarly, the top inlet/outlet 20 can be positioned at thevery top 18c of the tank 18 but may also be positioned at any place inthe top portion 18a of the tank 18. In one embodiment of the claimedinvention, the top portion 18a contains water that is in the range ofabout 60° F. (about 16° C.) to about 70° F. (about 21° C.). In anotherembodiment, the temperature of the water in the bottom portion 18b isjust above freezing temperature, which may vary depending uponatmospheric conditions (such as atmospheric pressure), or if chemicalsare added to the water. Preferably, the water in the tank is pure water.However, the claimed invention contemplates the addition of variouschemicals or other additives to the water to change the properties ofthe water mixture. Some chemicals, when added to water, tend to decreasethe freezing temperature of water. Other chemicals tend to change thedensity of water. Still others may change the viscosity or heat capacityof the water. It may be desirable to add a chemical such as sodiumnitrate to lower the freezing temperature of the water in the tank. Thisin turn may allow colder water to be delivered to the air chiller andcan protect the system from freezing. Alternatively, for on-line systemswhich may be subjected to freezing ambient temperatures, the use ofPotassium Formate is preferred instead of Ethylene Glycol or PropyleneGlycol to protect the water from freezing. Potassium Formate maintains alower viscosity than either of the glycols and thus gives better heattransfer at low temperatures. Potassium formate also has the addedadvantage of being more environmentally friendly than glycols. As usedherein, the term “water” refers to pure water or an aqueous mixtureincluding any additives.

The charge and discharge cycles will now be described with reference toFIG. 2A. The average temperature of the chilling water 16 in the tank 18is preferably lowered or raised during separate cycles. During the waterchilling or “charge” cycle, the average temperature of the water in thetank is lowered by introducing lower temperature chilling water 16a tothe bottom of the tank 18b from the water chilling system 13. In anadvantageous aspect of this invention, this charge cycle will typicallybe during the night-time or “off-peak” hours. At night, the ambienttemperatures are generally lower, thereby largely eliminating the needto chill the inlet air 15a, 15b. Further, at night there is usually lessdemand for the power being produced by the power turbine. Therefore, atnight, the water can be chilled using excess energy from the gas turbinesystem or power grid. Less electricity is required for primary powerusage, and less expensive parasitic power is available for running themechanical chiller 24. Also, more heat from the exhaust gas or steam maybe available for running the absorption chiller 26 since less steam maybe required by the steam turbine or cogeneration host during these“off-peak” night time hours. The charge cycle may, however, be performedat any time that proves advantageous to the particular operatingconditions of the gas turbine system. Generally, the charge cycle shouldbe performed when the need for useful power from the gas turbine systemis at a minimum, i.e. off-peak periods, while the discharge cycle shouldbe performed when the need for useful power is at a maximum, i.e.on-peak periods. As indicated above, after the charge cycle, thechilling water in the entire tank is preferably at a temperature ofabout 34° F. (about 1° C. to about 2° C.) to about 40° F. (about 4° C.to about 5° C.) unless additives are added to reduce the freezing pointin which case even lower temperatures could be used. During the chargecycle, warm water 16e is pulled from the top 18a of the tank 18 andpumped through the water chilling system 13. Chilled water 16a isintroduced back to the bottom portion 18b of the tank 18. The waterlevel in the tank 18 does not change, only the proportion of warm water16e to chilled water 16a changes as the tank becomes progressivelychilled. Preferably, by the end of the charge cycle, the averagetemperature of the water in the tank is about 33° F. (about 0° C. toabout 1° C.) to a range of from about 35° F. (about 1° C. to about 2°C.) to about 40° F. (about 4° C. to about 5° C.).

During the “discharge” cycle, all of the water chillers (e.g., chillers24, 26) may be turned off, so that all the chilled water requirementsfor the air chilling coil 14 may be supplied by the tank 18.Advantageously, the discharge cycle occurs during peak power usage times(e.g., during the day), when parasitic power is most costly and/or aninsufficient amount of waste heat from the exhaust gas 45 or steam mayto be available, e.g., to chill the water. As used herein, “day-time”refers to the period of time between sunrise and sunset. At this point,the storage tank 18 feature and the stored chilled water 16 in the tank18 become particularly advantageous. Preferably, sufficient chilledwater 16 is stored in the tank to last for the entire “discharge” cycle,with the option to have the water chilling system 13 supplement thestored chilled water 16 with directly chilled water as needed.Preferably, the amount of water discharged during the discharge cycle isless than the total volume of water stored in the tank 18. As before,chilling water 16b is removed from the bottom portion 18a of the tank18, through bottom inlet/outlet 22. The chilling water 16b then passeson towards the air chiller 14. (An optional additional mechanicalchiller 30 can be provided to further cool the chilled water 16b andintroduce further chilled water 16c to the air chiller 14) The chillingwater 16c then cools the inlet air in the air chiller 14 (e.g., aconventional air coiling coil), which produces higher temperaturechilling water 16d. This higher temperature chilling water 16d isreturned to the top portion 18a of tank 18. Because the highertemperature water 16d is being added to the tank 18, the averagetemperature of the water in the tank is increased (e.g., to a range offrom about 60 (about 16° C.) ° F. to about 70° F. (about 21° C.)).However, by virtue of the temperature gradient within the tank, and thestratified nature of the water therein (as discussed above), the highertemperature water occupies the upper portion 18a of the tank 18, leavingthe lower temperature water in the lower portion 18b of the tank 18,which is being discharged through outlet 22 to pass to the air chiller14. Eventually, over time, the line (the thermocline) between higher andlower temperature water gets lower and lower in the tank, i.e., itapproaches the bottom of the tank. Preferably, however, if the tank 18is large enough, before that line reaches the outlet 22 of the tank 18,the “charge” cycle is initiated, whereupon the water chillers (24, 26)are activated, introducing new chilled chilling water 16a to the tank.That new lower temperature chilling water then begins to fill up thebottom portion 18a of the tank 18. In one embodiment, it may bepreferable to initiate the charge cycle before the average temperaturein the tank reaches about 36° F. (about 2° C. to about 3° C.).

As indicated in FIG. 2A, a number of different types of water chillerscan be provided, at different locations, depending on design needs. Forexample, various mechanical chillers 24, 30 can be provided. Preferably,an upstream chiller is provided and whenever recovered GT exhaust heatis available, this upstream chiller is preferably an absorption chillerdriven by either steam 44 from the HRSG 38 and/or steam from the backpressure steam 46 from the steam turbine 40 exhaust or hot water orsteam 48 from an optional heat recovery coil 42. The use of absorptionchillers to pre-chill the highest temperature water returning from theair cooling coil or tank is preferred, so long as a low grade heatsource is available. This reduces the parasitic power required andimproves the heat rate (efficiency) of the gas turbine by utilizing whatwould otherwise be “waste heat” energy. By combining the use of thechilled water storage tank 18 with absorption chillers, the amount ofheat required can be made constant throughout a 24-hour day, even thoughthe demand for chilled water may vary greatly between daytime andnight-time. However, on most combined-cycle power plants where most ofthe gas turbine exhaust heat energy is already being used to providesteam to a steam turbine, the preferred upsteam chiller is a mechanicalchiller because the efficiency of the mechanical chiller as measured bythe coefficient of performance (COP=BTU of Refrigeration Duty/BTU ofEnergy required to drive the chiller) is much higher for the mechanicalthan the absorption chiller. The COP of a mechanical chiller is approx 6to 7, while the COP of a single stage absorption chiller is about 0.6and the COP of a two stage absorption chiller is about 1.0. Therefore byusing this steam in the steam turbine to produce additional electricalenergy and then using some of this electrical energy to drive amechanical chiller is a more efficient chilling systems than using thissteam in an absorption chiller.

Now, with reference to FIG. 2B, a preferred embodiment of the method andapparatus of the present invention will be discussed. In thisembodiment, multiple conventional gas turbine systems 12 are provided.Each gas turbine system 12 has an air chiller 14. One tank 18 is shown,however it may be desirable to use multiple tanks 18 depending upon theconfiguration of the plot space available. The inventor has found apreferred relationship between the amount of cooling required by the gasturbines and the volume of water that should be stored in the tank(s)18. This relationship is as follows:

$\frac{\left( {P \times C} \right)}{\Delta T} = \text{volume}$

Where: P=the total amount of cooling required to reduce the temperatureof the inlet air to the gas turbines 12, expressed in ton hours (eachton hour=12,000 BTU); ΔT=the difference in temperature of the water 16cand 16d across the air chiller 14, expressed in ° F.; C=a constantexpressed in (° F.*gallons)/(ton*hours); and volume=the total volume ofstored water required in gallons. The constant C is a number that isdetermined according to various required tank design parameters, such asthe required height of the tank, the ΔT of the water and the diffuserdesign. Generally, C is in the range of about 1600 to about 1750;preferably C is in the range of about 1700 to about 1725; and in onespecific embodiment, C was determined to be about 1720.

Depending upon the space requirements or soil conditions of any giveninstallation, it may be preferable to employ several small tanks 18, orone larger tank 18. The design choice also depends upon the type offoundation chosen to hold the tank 18. Preferably, a ring-wallfoundation is used, as shown in FIG. 3. In an embodiment with severaltanks 18, each tank preferably has a bottom inlet/outlet 22 and a topinlet/outlet 20 and would preferably operate in much the same manner aspreviously described. Generally, tank volume requirements range from800,000 gallons to 10 million gallons. Tank heights range from 25 feetto 70 feet, or to 90 feet. Tank diameters range from 50 feet to 250feet. Normally, the tank diameter is greater than its height. Sometimes,it is preferred to have charge/discharge cycles that are relativelyshort in duration. For example, it may be more economical to employ atank 18 that is only large enough to hold a volume of water for adischarge cycle lasting 4 or more hours. It also may be preferred tohave a larger tank to hold a volume of water for an 8 or a 12 or morehour discharge cycle. Although generally for these longer peak periodsthe tank would supplement the chillers in a “partial storage” operationto maximize the available on-peak cooling hours with a given tank size.Generally, tank volumes range from 800 thousand gallons to 10 milliongallons, but again, the volume of the tank is related to the ton-hoursof cooling required to meet the desired entering air temperature of thepower turbine which is a function of the ambient air enthalpy, thedesign chilled turbine inlet temperature, the airflow rate of theparticular GT, the number of GT's, and the number of hours/day thestorage system is to provide chilling.

B. Additional Methods and Systems

As discussed in the summary above, one or more embodiments of theinvention include methods of chilling inlet air for a gas turbine powerplant. The methods may include the use of features in addition to thoseshown in FIGS. 1-4. If a thermal storage tank is not used, the systemwill normally operate as an “on-line” system, meaning the chillersprovide the chilling required by the coils and are operating at the timethe coils use chilled water. One or more embodiments of the methodinclude passing inlet air through a cooling coil, preferably amulti-pass cooling coil that includes at least four passes. The coolingcoil should include an opening for receiving the inlet air and ispreferably operably connected to a gas turbine power plant that includesat least one gas turbine, at least one compressor and at least one gasturbine inlet which receives the inlet air. The method may also includepassing circulating water through one or more water chillers (which arepreferably sequentially positioned) at a first flowrate to reduce thetemperature of the circulating water, e.g., from a first temperature toa second temperature. Each water chiller should include at least oneconduit, e.g., a piping or other tubular arrangement, through which thecirculating water is capable of passing. The method preferably alsoincludes passing the circulating water having the first flowrate, e.g.,a relatively higher flowrate, through the cooling coil in an amountsufficient to lower the temperature of the inlet air to the desiredtemperature during high ambient (design conditions). Then, in apreferred embodiment of the invention, the method includes reducing theflowrate of the circulating water passing through the water chiller,e.g., to a reduced flowrate, e.g., a second flowrate during lowerambient (off-design conditions). Then, that preferred method should alsoinclude passing the circulating water through one or more water chillers(preferably the same water chillers corresponding to the first flowrate)at a different or “reduced” or “second” flowrate, in such a way and inan amount to increase the temperature difference (ΔT) between thecirculating water entering the cooling coil and the circulating waterleaving the cooling coil. The second flowrate should be lower than thefirst flowrate. Accordingly different predetermined flowrates for waterpassing through two or more chillers can be used. Then, the methodshould also include passing the circulating water having the secondflowrate (or the reduced or different flowrate) through the cooling coilin an amount sufficient to lower the temperature of the inlet air.Preferably, the circulating water having a flowrate reduced as discussedabove is passed through two or more sequentially positioned waterchillers, and the circulating water is then directed through amulti-pass cooling coil. Preferably the circulating water having thefirst (e.g., higher) flowrate should be reduced to the second (lowerflow rate) once the water ΔT (e.g., a temperature reduction by two ormore sequentially positioned water chillers) is reduced to apre-determined point due to a reduction in ambient load.

Alternatively, one or more embodiments of the invention include a methodof chilling inlet air for a gas turbine power plant that includes one ormore of the following aspects. In one or more embodiments, the methodcomprises passing inlet air through a cooling coil that is preferably amultipass cooling coil with four or more passes and that includes anopening for receiving inlet air and that is operably connected to a gasturbine power plant, i.e., directly or indirectly connected. That methodmay also include passing the inlet air (after being cooled) through atleast one gas turbine inlet. That method preferably also includespassing circulating water through a water chiller (preferably two ormore in-series chillers) to reduce the temperature of the circulatingwater (FIGS. 1 and 4). Each water chiller preferably includes at leastone inlet for receiving circulating water, at least one conduit throughwhich the circulating water is capable of passing, and at least oneoutlet for dispensing circulating water. The circulating water should bepassed through two or more sequentially positioned compressors forsequentially chilling the circulating water. These compressors can bepart of two different water chillers or part of a single duplex chiller.As used herein, a “duplex chiller” is a mechanical device with at leastone inlet and at least one outlet where the temperature of water passingthrough the device is reduced two times via two different refrigeranttemperatures and two separate compressions. Then, that preferred methodshould also include passing the circulating water through the coolingcoil in an amount sufficient to lower the temperature of the inlet air,e.g., by making heat transfer contact between the circulating water andthe inlet air. The “amount sufficient” is determined by specific systemneeds such as capacity, cooling coil feed air wet bulb temperature, andthe desired leaving air temperature set-point. In addition, thepreferred method should include reducing the flowrate of the circulatingwater passing through the two or more sequentially positioned waterchillers during reduced load ambient conditions. Also, the preferredmethod includes passing the circulating water having the reducedflowrate through the cooling coil in an amount sufficient to lower thetemperature of the inlet air preferably by directly passing to a coolingcoil, the water e.g., all or substantially all of the water, exiting thelast (furthest downstream) water chiller prior to the cooling coil.Preferably, in most cases, the circulating water is not diverted orsplit as it passes between the water chillers and the cooling coil,e.g., by directing any portion (or more than 25% or 50%) of it to thewater returning back to the chillers.

Another specific embodiment of the invention includes a method ofchilling inlet air for a gas turbine power plant that includes one ormore of the following aspects. For example, the method may includepassing inlet air through a cooling coil. The method may also includepassing circulating water through a water chiller to reduce thetemperature of the circulating water. In addition, the method shouldalso include passing the circulating water through the cooling coil tolower the temperature of the inlet air and to provide chilled inlet airto the gas turbine power plant. The method may additionally includesupplying water to the chilled inlet air in an amount sufficient toincrease the moisture content of the chilled inlet air, e.g., by addingwater, e.g., liquid water or water vapor, to the inlet air after theinlet air has been treated partially or completely by the cooling coil,i.e., made at least partial heat transfer contact.

All references herein to “circulating water” refer broadly to anyportion or all of the circulating water being used in the system,although in certain cases it will be apparent from the context that areference to “circulating water” refers only to a selected portion ofthe circulating water in the system (e.g. when the temperature of aparticular portion of circulating water is reduced, in which case thetemperature of other portions of circulating water in other parts of thesystem may not necessarily be reduced). Preferably, the circulatingwater discussed herein travels in a complete “loop” as shown in FIG. 4,so that the same water is repeatedly cooled and heated.

Variable Flow and Low Flow. An important aspect of certain embodimentsof the invention includes reducing the flowrate of circulating water ina particular way. All references to “flowrate” herein refer to the rateof circulating water passing through a particular portion in the system,e.g., the pump (e.g., in gpm), divided by a given amount ofrefrigeration duty (e.g., in tons). Preferably, optimizing the propergpm/ton is an important design criteria. It is desirable to vary thechilled water flowrate to maintain a relatively low gpm/ton ofapproximately 0.3, 0.4, 0.5, 0.6, 07 or 0.8 to 1.6, 1.7, 1.8 or 1.9gpm/ton at full load throughout the operating ambient range. The optimumdesign for on-line cooling systems will be from about 1.4 gpm/ton toabout 1.0 gpm/ton. The optimum design for thermal storage systems willpreferably be from 1.2 to 0.6 gpm/ton at full load. In addition it isdesirable to vary the chilled water flowrate to maintain a relativelylow gpm/ton of approximately 0.6 to 4 gpm/ton throughout the part-loadoperating ambient range or more preferably to maintain a flow of approx0.8 to 2.5 gpm/ton. This will save significant pump power during thepart load operation and it will also maintain a relatively warm returnwater temperature thus maintaining a high efficiency on the upstreamcompressors. More specifically, one or more embodiments of the inventioninclude reducing the flowrate of circulating water passing through twoor more sequentially positioned water chillers, preferably two duplexchillers (which provide four different temperature reductions), andpassing the circulating water having the resulting reduced flowratethrough a cooling coil in an amount sufficient to lower the temperatureof the inlet air (FIG. 4). In other specific embodiments, a method ofchilling inlet air includes passing circulating water, having a firsttemperature, through a pump, e.g., at a first flowrate, then passingthat same water through a water chiller that reduces that circulatingwater temperature (e.g., using a first compression) so that thecirculating water has a second temperature, which is lower than thefirst water temperature, and then passing that water through a secondwater chiller to reduce the circulating water temperature from a secondtemperature to a third temperature (e.g., using a second compression)that is lower than the second.

In a specific embodiment of the invention, the method includes reducingthe circulating water flowrate in response to certain predeterminedsetpoints or events, i.e., criteria or benchmarks, e.g., in response topredetermined decreases in ambient air wet bulb temperature or enthalpy.As used herein, references to “ambient wet bulb temperature” refer tothe wet bulb temperature of the air entering the cooling coil at the gasturbine power plant intake. Accordingly, ambient wet bulb temperaturetends to constantly change at a given power plant location during theday and night, i.e., over a 24-hour period.

In a preferred embodiment, reducing the circulating water flowrate isbased on a setpoint, which is discussed in further detail below. In apreferred embodiment where the chilled air temperature (e.g., compressorinlet air) is desired to be constant, the setpoint is a function of bothambient wet bulb temperature of the air and the temperature differencebetween the circulating water entering the cooling coil and thecirculating water leaving the cooling coil (water ΔT). As the ambientwet bulb temperature decreases, the heat transferred to the circulatingwater from the inlet air also decreases. The water ΔT also decreasessince the water ΔT is dependent upon heat transfer contact with theinlet air within the cooling coil. As the ambient temperature decreases,the temperature of the inlet air entering the cooling coil alsodecreases; therefore, the circulating water temperature can increaseslightly and still maintain a desired leaving air temperature. Theleaving air temperature remains constant because the load (Q) on thecooling coil decreases and thus the required log mean temperaturedifference (LMTD) between the air and the circulating water is reduced.As a result of the reduced ambient wet bulb temperature and thus thereduced load, the heat transfer between air and circulating water in thecooling coil decreases, resulting in a decreased water ΔT, as shown inthe following equations:(mΔh)_(A)=[(mCp)(T₀−T₁)]_(w)Q=mCpΔT=mΔhQ_(coil)=UA(LMTD);As shown above, when the Δh of the air is reduced, the ΔT of the wateris also reduced when the mass flowrate (m), the temperature of the airleaving the cooling coil (T_(oa)), and the heat transfer coefficient(C_(p)) remain nearly constant. The air leaving the cooling coil istypically saturated, i.e., the air has about a 100 percent relativehumidity, therefore the wet bulb temperature and dry bulb temperaturesof the leaving air are substantially the same.

In a preferred embodiment of the invention, a high system efficiency isachieved by maintaining a high water ΔT, rather than a high circulatingwater flowrate. Preferably, achieving a high system efficiency at a lowcirculating water flowrate (e.g., about 1 gpm/ton) depends, in part, onreducing the temperature of the circulating water at least two timesbefore it chills the inlet air, i.e., sequential chilling. A preferredembodiment of the method includes using at least two water chillers tosequentially chill the circulating water.

As shown above, the traditional chilled water designs which utilize ahigh flowrate, e.g., from about 2 gpm/Ton to about 1.5 gpm/Toncirculating water flowrate at full load results in a lower circulatingwater ΔT (from 12° F. ΔT to 16° F. ΔT respectively) resulting in colderwater (e.g., from about 52° F. to about 56° F. respectively) waterreturning to the upstream chiller. For example, the GE LM6000 isprovided with a cooling coil that has been optimized for inlet coolingof their turbine. This coil is designed for a maximum design ambientcase of 2200 tons of cooling using 3300 gpm of circulating chilled waterflow. This equates to 1.5 gpm/ton or a 16° F. ΔT. This chilled water ΔTwill get proportionately smaller as the ambient temperature drops belowdesign because the flow rate (gpm) remains constant in conventionaldesigns while the load (tons) is fluctuating with the ambienttemperature. A preferred embodiment of the present invention includesreducing the circulating water flowrate to provide or maintain a higherwater ΔT. It has been discovered that in the specific context describedherein, reducing the circulating water flowrate reduces the amount ofheat transfer through the cooling coil, i.e., heat transferring from theinlet air to the circulating water passing through the cooling coil. Asshown in the above equations, a lower circulating water flowrate resultsin higher water ΔT when the inlet air flowrate and air Δh remainconstant. As a result, the temperature of the circulating water leavingthe cooling coil is higher at a lower flowrate than at a higherflowrate, thereby resulting in a high water ΔT. The use of sequentialcooling via series chillers and/or multiple compressors allows highupstream compressor efficiency as a result of relatively warmerrefrigerant temperatures. The warmer refrigerant temperatures arepossible because the circulating water returning from the cooling coilis warmer. In addition, the power required to drive the circulatingwater pump will be lower since the power consumption required isproportional to the circulating water flowrate cubed.

In certain embodiments of the invention, the circulating water flowrateis reduced to maintain the chilled water ΔT within a specific designrange. This ΔT should be maintained within a range of about 40° F. to16° F. to maintain maximum efficiency with a sequential chilling systemwith the higher end of this range being better for thermal storageapplications & high ambient climates. The lower end of this range isbetter for on-line applications with moderate ambient climates. Inanother specific embodiment, the leaving chilled water temperaturesetpoint and the circulating water flowrate setpoint may be changed tomaintain the leaving air temperature and the chilled water ΔT within thedesign parameters. As used herein, the term “setpoint” refers to anypredetermined point or event that results in the flowrate through thechillers and the coil being changed, or a change in the temperature ofthe water leaving the chiller. The setpoint may be or include apredetermined air Δh, or change in wet bulb temperature across the coilor the setpoint may be a predetermined ambient temperature or change intemperature or the setpoint may be a change in chilled watertemperature. In addition, the setpoint may be derived from inputparameters such as the chilled H₂O flowrate and chilled H₂O Δh. Thesetpoint may be changed depending on the time of the day or depending onsystem needs or the ambient temperature. As used in preferredembodiments herein, the “setpoint” is based upon maintaining a chilledwater ΔT of at least 16° F. It is believed that the characteristics of aparticular system are primarily determined by the wet bulb temperatureof the ambient air and the leaving air temperature since this determinesthe load on the coil and also determines the temperature of the coolingtower water going to the chiller. As used herein, the term “wet bulbtemperature” refers to the temperature measured by a thermometer withits bulb wrapped in wet muslin, although the wet bulb temperature mayalso be measured by any means known to those skilled in the art but mostcommonly is calculated electronically by simultaneously measuring drybulb temperature and relative humidity. Preferably, the wet bulbtemperature is electronically calculated by simultaneously measuring thedry bulb temperature and the relative humidity of the air. The wet bulbtemperature is typically lower than the dry bulb temperature because thewater on the bulb evaporates, resulting in cooling. Therefore, thedifference between wet bulb temperature and dry bulb temperature dependson the humidity in the air. In carrying out certain specific embodimentsof the method, the wet bulb temperature of the inlet air leaving thecooling coil is equal to its dry bulb temperature, in which case the airis considered to be “saturated” or 100% R.H.

In one or more specific embodiments of the invention, the circulatingwater is passed through at least one pump to vary the flowrate of thecirculating water before it is subjected to sequential chilling, e.g.,using two in-series chillers as shown in FIGS. 1 and 4. Alternatively oradditionally, the circulating water may be passed through any number ofpumps. Preferably the pumps are generally mounted in parallel to allowthe flow to be changed by sequencing a combination of pumps on and off.Preferably, at least a portion of the circulating water is passedthrough one centrifugal pump, e.g., a horizontal split case pump, and adifferent portion of circulating water is diverted and passed through atleast one additional pump the output streams of the two or more pumpsthen being combined. More preferably, the circulating water is split,then passed through two or more centrifigal pumps in parallel, thencombined. Optionally, one or more of the pump motors may be wired to aVariable Frequency Drive for greater flexibility in flow control andgreater partial load efficiency. The circulating water may be passedthrough a pump anywhere in the system. Preferably, however, as shown inFIG. 4, the circulating water is passed through at least one pump 60,referred to as a primary pump, located in the piping that circulates thechilled water through the chillers. Although the circulating waterflowrate is preferably varied only at the primary pump, the circulatingwater may additionally or alternatively be passed through other pumps atany location in the system. When circulating water is passed throughthose other pumps, those pumps are typically not used to reduce thecirculating water flowrate through the water chillers, but rather areused for another purpose, such as to pass water from a bank of chillersto the cooling coils.

In a preferred embodiment, the circulating water passes through at leastone pump at full flow when the ambient wet bulb temperature is at amaximum (e.g., from about 72° F. to about 87° F.), typically at somepoint in time between noon and 3:00 pm during the summer season. As usedherein, the term “full flow” refers to the maximum circulating waterflowrate of the system. In this particular embodiment, when the ambienttemperature drops (e.g., to a lower wet bulb period such as during themorning or afternoon) the water ΔT also drops. When the chilled water ΔTreaches a first setpoint (e.g., from about 75% to about 50% of designΔT), one of the centrifugal pumps is preferably turned off. Shutting offone of the two operating centrifugal pumps should accordingly reduce thecirculating water flow rate from about 100 percent flow to about 70percent flow, thereby increasing the water ΔT, e.g., by about 43percent. Then, when the circulating water reaches a secondsetpoint(e.g., from about 75% to about 50% of design ΔT), the VFD on thefirst VFD pump is reduced, further reducing the circulating waterflowrate enough to maintain the chilled water ΔT to at least about 16°F.

Water Chilling. Another important aspect of one or more specificembodiments of the invention includes reducing the temperature of thecirculating water from an initial temperature, e.g., a firsttemperature, to an intermediate temperature, e.g., a second temperature,that is lower than the initial temperature, e.g., first temperature, andthen further reducing the circulating water from the intermediate, e.g.,second, temperature, to a final temperature, e.g., a third temperature,that is lower than the intermediate temperature, e.g., secondtemperature. In the aforementioned method, the circulating watertemperature may thus be reduced in stages by passing circulating watersequentially through two or more water chillers. An example is shown inFIG. 4, which shows circulating water passing from a cooling coil 54 toa first water chiller 62, then to a second water chiller 64, thenthrough an optional third chiller 66 and fourth chiller 68, and thenback to the cooling coil 54. As used herein, the term “water chiller”refers to an apparatus for lowering the circulating water temperaturethat includes at least a single compressor. Preferably the water chillerincludes at least one opening for receiving the circulating water, atleast one outlet for dispensing the circulating water. A conduit throughwhich the circulating water is capable of passing should operablyconnect the one opening for receiving circulating water with the oneoutlet for dispensing circulating water. Preferably, the circulatingwater is passed through at least two water chillers, which can form partof a single “duplex chiller,” although it could alternatively consist oftwo simplex chillers with the evaporators piped in series. Preferably,at least a portion of the circulating water is passed from and throughthe first water chiller to and through the second water chiller. Morepreferably, all, or substantially all, of the circulating water ispassed from and through the first water chiller to the second waterchiller.

Passing the circulating water through a water chiller, e.g., aconventional mechanical or absorption chiller, reduces the circulatingwater temperature. When the circulating water is sequentially passedthrough two water chillers whose evaporators are piped in series (orthrough a single duplex chiller), the circulating water temperature isreduced twice. Preferably, in carrying out certain methods of theinvention, the sequential circulating water temperature reductions areaccomplished by passing the circulating water through a duplex chillersuch as the Trane duplex centrifugal CDHF water chiller. As shown inFIG. 4, staged or step-wise circulating water temperature reductions canbe accomplished by passing circulating water 58 through an evaporator62a within the duplex chiller CH2. The evaporator chills the circulatingwater by receiving a refrigerant such as ammonia, R-22, R-134a, or R-123available from Dupont. Preferably, R-123 or a similar refrigerant ispassed from a condenser 62b to the evaporator 62a to chill the incomingcirculating water. The refrigerant is then passed from the evaporator62a back through a compressor 62c to the condenser 62b for condensingthe vaporized refrigerant back to a liquid. The refrigerant is cooledand condensed by condenser water 72a passed from a cooling tower 70 tothe condenser 62b (typical of one chiller).

A specific embodiment of the invention includes passing circulatingwater through a duplex chiller to reduce its temperature from a firsttemperature to a second temperature lower than the first, then to athird temperature lower than the second (FIG. 4). The circulating watercan then be passed through another duplex chiller to further reduce thewater temperature twice. Any number of water chillers may be included toreduce the temperature of circulating water for large tonnageapplications on large gas turbines (above 60 MW) in a greater number ofsequential steps although two duplex chillers in series (4 stages ofcooling) is considered the optimum. For larger gas turbine installationsthat would require more capacity than can be accomplished with 2 duplexchillers, additional pairs of duplex chillers can be provided thatdivide the total flow of water into the parallel trains of chillers(similar to the 2 parallel trains shown in FIG. 4).

The discussion of the embodiments has focused primarily on thesequential chilling of the chilled water by using progressively colderevaporator refrigerant temperatures. However, there is also increasedefficiency available by utilizing sequential heat rejection from therefrigerant to the condenser water through two or more condensers inseries. It is preferred that the condenser water be piped in acounterflow arrangement to that of the chilled water, i.e., the coldestcondenser water is adjacent to the coldest circulating water.

Sequential chilling of the circulating water in the evaporator, whichresults in sequential vaporization of the refrigerant, can be combinedwith sequential heating of the cooling tower water, which results insequential condensing of the refrigerant, thereby equalizing the head oneach compressor, e.g., by passing all, substantially all, or at least aportion, of circulating water from a first water chiller to a secondwater. Equalizing the head on each compressor can increase thecompressor efficiency, shown in greater detail below. As used herein,the term “head” refers to the compressor pressure ratio, which is thepressure of the condenser divided by the pressure of the correspondingevaporator. For example, referring to FIG. 4, the upstream compressor62c head is equal to the pressure of the upstream condenser 62b dividedby the pressure of the corresponding Evaporator 62a.

In a preferred embodiment of the invention, the circulating water ispassed from a cooling coil through two duplex chillers (CH 2 & CH 4),sequentially. The circulating water passing through the duplex chillersis reduced from a high temperature resulting from a high water ΔTthrough the cooling coil (from about 55° F. to about 70° F.) to a finaltemperature of from about 34° F. to about 44° F., that is the coldest inthe system. Example data in such a system is shown in Tables 1 and 2 andFIG. 7.

TABLE 2 Circulating Water Circulating Water Inlet Outlet TemperatureTemperature (° F.) 58_(b) (° F.) 58_(a) Temperature Profile throughWater Chillers at 6600 gpm (full flow) & Full Load (75 F. Ambient WetBulb Temp) chilled to 50 F. T2 Air Temp First Water Chiller 62 61.5 F.55.6 F. Second Water Chiller 64 55.6 F. 50.5 F. Third Water Chiller 6650.5 F. 45.6 Fourth Water Chiller 68 45.6 41.4 Temperature Profilethrough Water Chillers at 4620 gpm (70% of full flow) & Part Load (70 F.Ambient Wet Bulb Temp) & 50 F. T2 Temp First Water Chiller 62 62 F. 55.5F. Second Water Chiller 64 55.5 F. 50.0 F. Third Water Chiller 66 50.0F. 44.6 F. Fourth Water Chiller 68 44.6 F. 40 F.

One benefit of sequentially chilling the circulating water is that onlythe downstream compressor 68c needs to compress the refrigerant to a lowenough pressure to chill the circulating water to the lower leavingchilled water temperature which is required with a lower circulatingwater flowrate (FIG. 4).

When the circulating water flowrate is reduced, the power consumption ofthe downstream compressor may increase. The compressor power consumptionincreases as a result of chilling the refrigerant to a lower temperaturedue to the lower leaving water temperature than that required at a highcirculating water flowrate. The circulating water entering thedownstream evaporator is at a higher temperature than when circulatingwater is at full flow because the coil will heat up the circulatingwater more at lower flow. Therefore, at a reduced flowrate, thedownstream refrigerant must be at a lower temperature to maintain therequired LMTD and heat transfer required at the cooling coil.

An alternative, when water is unavailable for use in a water-cooledcondenser, an air-cooled condenser may be used to reject the heat fromthe refrigerant to the ambient air An air-cooled condenser typicallycannot be used to sequentially reject heat to the ambient like that ofseries piped water-cooled condensers, but it will still provide anincrease in the upstream compressor efficiency as a result ofsequentially chilling the circulating water using staged evaporators toallow sequentially lower refrigerant temperatures with the differentcompressors. A preferred embodiment of this invention is to combinesequential chilling of the circulating water with a chilled waterthermal storage tank as discussed earlier. This is especially beneficialwhen no water is available due to the great variability in the dry bulbtemperature between daytime and nighttime. The lower nighttime dry-bulbtemperature will significantly increase the capacity and the efficiencyof the chillers to generate chilled water off-peak and minimize thedaytime on-peak parasitic power required.

Air Chilling. Another important aspect of the invention includesreducing the temperature of the inlet air, which may include passingcirculating water through a cooling coil in an amount sufficient toreduce the temperature of the inlet air. The reduction in inlet airtemperature increases the density of the air, allowing a higher massflow rate through the compressor of the gas turbine power plant.Therefore, a higher mass flowrate allows the gas turbine power plant toproduce more electricity.

In specific embodiments of the invention, the circulating water makesmore than one pass through the cooling coil. Most preferably, thecirculating water makes four or more passes through the cooling coil. Ina specific embodiment shown in FIG. 5, the circulating water is passedthrough the cooling coil 54 six times which is the preferred method if athermal storage tank in used with a high ambient climate. As usedherein, the term “pass through the cooling coil” refers to each timethat the circulating water changes directions inside the cooling coil.Passing circulating water through the cooling coil four to six timesachieves a very high water ΔT (from about 20° F. to about 40° F.). Inaddition, four or six passes achieves good heat transfer at low waterflow rates between the circulating water and the inlet air due to theturbulence of the water in the tubes. On each pass, the temperature ofthe circulating water is increased. For example, on the first pass 82a,the circulating water temperature may increase from about 39° F. toabout 44° F. The circulating water temperature may increase from about65° F. to about 74° F. on the final pass, 82f. Example data in such asystem is shown in Table 3.

TABLE 3 Temperature Profile through cooling coil at 0.69 gpm/TonCirculating Water Circulating Water Temperature entering Temperatureleaving pass (° F.) pass (° F.) First Pass 82a 39.00 44.04 Second Pass82b 44.04 48.94 Third Pass 82c 48.94 53.53 Fourth Pass 82d 53.53 58.72Fifth Pass 82e 58.72 65.40 Sixth Pass 82f 65.40 74.00

Passing inlet air through a cooling coil including multiple circulatingwater passes provides a significant reduction in the inlet airtemperature (from about 80 to 125° F. to about 43 to 60° F.). The inletair may be passed through any number of cooling coils as required toprovide enough face area to keep the air velocity through the coil atbetween 400 to 650 ft/min. Preferably, the inlet air is passed through asingle coil in the direction of airflow to the gas turbine power plantbut it may also flow through a second coil if required to get the highdelta T desired. More preferably, the circulating water is passedthrough only one cooling coil in the direction of airflow with multiplecoils placed above or on the side as needed to provide sufficient facearea.

Water Addition. In another embodiment of the invention, water may beadded to the inlet air after it has been chilled at least to someextent. Preferably, water is added to the compressor feed air, which isthe inlet air after it passes through and exits the cooling coil, i.e.,no longer contacts the coil, and before the inlet air enters, i.e.,first contacts, the turbine power plant compressor. Such compressor feedair is typically the coldest inlet air in the system. Preferably, thewater is added in the form of finely atomized water droplets or mist.Adding water to the compressor feed air provides (supplies) entrainedwater to the inlet air. As used herein, the term “entrained water”refers to water trapped within the air that does not evaporate. Thewater in the inlet air does not evaporate when the cooled inlet air,e.g., the condenser feed air, is already fully saturated, i.e., at“saturation,” as a result of being chilled by passing through thecooling coil. Entraining water in the compressor feed air providescooling in the interstages of the compressor within the gas turbinepower plant. The compressor intercooling occurs as the inlet air passesthrough the compressor. As the inlet air passes through the compressorand is compressed, the inlet air is heated, thereby vaporizing theentrained water. The heat absorbed by the vaporization of the liquidmist into water vapor cools the air in the compressor. Intercooling ofthe compressor can increase the compressor efficiency and may improvethe power output by approx 140 KW per gallon of water added per minute.Thus, any of the methods described herein for cooling inlet air mayadvantageously further include the addition of water as described above.

Although the water may be added to the chilled inlet air from anysource, e.g., from a vessel such as the storage tank, water ispreferably added from the cooling coil condensate 70, as shown in FIG.4. As used herein, the term “cooling coil condensate” refers to watercondensed out of the inlet air, e.g., the air stream passing through thecooling coil. Adding cooling coil condensate, rather than water fromanother source, utilizes water that is already available. The water maybe added to the inlet air at any location. Preferably, the water isadded before the inlet air enters the gas turbine power plant 76 butafter it leaves the cooling coil 54. Alternatively, this water may bestored and used when the chilling system is off but the gas turbine isstill operating by providing an evaporative cooling effect.

Heating. In another embodiment of the invention, the circulating wateris passed from the cooling coil 54 to the heater 84 and back to thecooling coil, as shown in FIG. 4. For example, the circulating water canbe passed to the heater on cold days (e.g., when the ambient temperatureis below about 10° F.). The circulating water is heated from about 10°F. to about 20° F. to prevent icing of the turbine within the gasturbine power plant. This may be particularly useful on certainaeroderivative gas turbines such as the LM6000. Any heater may beincluded, e.g., gas fired or electric water heater of steam or hot waterexchanger. Passing the circulating water through a heater may increasethe efficiency of some gas turbines during very cold periods (whenambient temperature is below about 30° F.). For example, some turbineshave a limit on the amount of mass flow they can accept due to theircompressor design such as some of the Westinghouse 501F models. Duringvery cold ambients these turbines must use Inlet Guide Vane control orother means to limit the mass flow of air into the compressor. Sincethis tends to be a less efficient operating point, it would beadvantageous to warm the air to reduce the density of the air and thuskeep the engine within a desirable mass flow range.

Circulating Water Additives. Any of the methods described herein mayinclude adding one or more additives to the circulating water to eitherprotect the circulating water from freezing or to allow coldercirculating water supply temperatures (from about 28° F. to about 35°F.). Any additive may be added, including glycol. Preferably, an organicor inorganic salt is added. More preferably, sodium nitrate is added toprevent the detrimental effects of glycol on the heat transferproperties and viscosity of water, which tend to increase the powerrequirements for pumping and for the chiller compressor. In addition,sodium nitrate is not corrosive like other salts. Sodium nitrate wouldbe the most preferable additive if a chilled water thermal storage tankwere used due to its low cost. However for on-line systems where nothermal storage tank is used, the most preferable additive is potassiumformate. The ability of potassium formate to protect the coil and pipingfrom freezing during winter ambients, combined with its excellent heattransfer properties and low viscosity at low temperatures makes this anideal additive for closed loop chilled water systems in Turbine InletCooling applications.

Packaging. The chilling system may be installed by any method, butpreferably, the system is mounted on a prepackaged factory built skid.The entire skid is enclosed, climate controlled and equipped with anoverhead monorail crane to facilitate maintenance.

In addition, the skid package would optionally include all of the motorstarters for the chillers and pumps. An optional heat rejection systemmay also be provided which would include one or more cooling water pumpsto circulate water from a cooling tower through the condenser tubes ofthe chiller and then carry the heated water back to the cooling tower,if water is available. A packaged cooling tower may optionally beprovided as part of the system and would preferably be mounted above theskid to minimize footprint and provide sufficient net positive suctionhead to the circulating water pumps mounted on the skid to prevent anycavitation with the pumps. Alternatively, for sites with waterrestrictions, an optional air-cooled condenser may be provided and wouldpreferably be mounted above or along side the skid. Additionally anoptional variable frequency drive may be mounted on the skid to modulatethe flow of water through the evaporator of the chillers, which wouldresult in lower energy consumption during reduced ambient periods. Thisoptional VFD may also be applied to the cooling tower fans and thecooling water pumps. The skid may include one or more water chillers,one or more chilled water pumps capable of varying the flow ofcirculating water through the evaporator tubes of the chillers, and acontrols system to optimize and control the proper amount of chilledwater flow and temperature to minimize the total amount of electricityrequired to power the inlet chilling system. The skid may incorporate amicroprocessor or PLC based controls system responding to temperaturesensors and flow measurement. This system may communicate with the powerplant's control system. The skid control's system could enable theturbine operator to monitor remote sites from a single location viamodem or internet communication.

Optimized Efficiency Control vs Optimized Capacity Control. Normally thecontrols of the Turbine Inlet Cooling system will be designed to providea constant inlet air temperature to the compressor of the gas turbine tomaintain its capacity during high ambient periods. This compressor inletair temperature (normally called “T2”) is typically maintained at asetpoint of approximately 45° F. or 50° F. to maintain the gas turbinemanufacturers minimum temperature to prevent icing in the bellmouth ofthe turbine. For simple cycle gas turbines (i.e, no steam turbine) thislower T2 air temperature also results in greater gas turbine efficiency(defined at BTU/KWH) as well as increased capacity (defined as KW orMW). However, for combined cycle plants, it has been found throughmodeling the plant operations with computer simulation software, thatthe overall heat rate (efficiency) of the plant goes down slightly whenreducing T2 utilizing Turbine Inlet Cooling even though the capacityoutput is significantly increased. This is because the colder inlet airto the gas turbine increases the mass flow and results in lowertemperature exhaust and thus lower steam pressure at the Heat RecoverySteam Generator (HRSG). This results in a lower percentage increase ofsteam turbine output vs the gas turbine output when compared to the sameplant at higher entering air temperature. This fact combined with theparasitic power required to drive the mechanical chilling system willusually result in a slight decrease in overall combined cycleefficiency. This efficiency degradation can be mitigated through the useof a special control algorithm whereby the inlet air dry bulbtemperature and relative humidity are precisely measured and the dewpoint calculated. By controlling the leaving air temperature off thecooling coil to maintain a temperature slightly above the dew pointtemperature, the coil can be prevented from producing condensate whichwill greatly reduce the parasitic power associated with the mechanicalinlet chilling system. An alternative method that accomplishes the samething would employ an accurate relative humidity sensor downstream ofthe coil and limit the leaving air temperature to where the RH ismaintained at about 95-99% and not allowed to become fully saturatedwhereby moisture would be condensed on the coil (see FIG. 6Psychrometric Chart). This reduced parasitic power will allow theoverall combined cycle plant to maintain its original high netefficiency and still get much of the capacity improvement associatedwith inlet cooling. This method of control will normally only beemployed when the economics of operating the power plant favor maximumefficiency over maximum capacity.

1. A method of chilling inlet air to a combined cycle gas turbine plant,comprising: a. a gas turbine plant that includes a gas turbine and a gasturbine air inlet and a steam turbine; b. providing a system ofcirculating liquid chilling water including a chilling system thatincludes a first chiller; c. providing a storage tank which is operablyconnected to the chilling system, the storage tank containing a columnof water characterized by a top and a bottom; c.d. removing water fromthe storage tank, passing at least a portion of the liquid chillingwater through the first chiller, the liquid chilling water passingthrough the first chiller being lowered to a first temperature and thenintroducing at least a portion of the removed water into the watercolumn, wherein the average temperature of the water in the storage tankis lowered; d.e. providing an inlet air chiller, comprising a coolingcoil through which liquid chilling water passes, for lowering thetemperature of inlet air being fed to the gas turbine compressor throughheat transfer between the liquid chilling water passing through thecooling coil and the inlet air, wherein the inlet air chiller provides aliquid chilling water temperature rise; e.f. chilling the inlet air byremoving water from the water column and then directing the liquidchilling water through the cooling coil of the inlet air chiller to makeheat transfer contact between the liquid chilling water and the inletair; and f.g. controlling the leaving air temperature off the coolingcoil to maintain a leaving air temperature slightly above the dew pointtemperature of the ambient air to maintain high efficiency on the powergas turbine plant.
 2. The method of claim 1, wherein an amount ofcirculating chilled water flow rate is varied to the cooling coil tomaintain a leaving air temperature slightly above the dew pointtemperature of the ambient air.
 3. The method of claim 1, wherein thetemperature of the circulating chilled water is varied to the coolingcoil to maintain a leaving air temperature slightly above the dew pointtemperature of the ambient air.
 4. The method of claim 1, wherein acirculating chilled water flow rate or the circulating chilled watertemperature is varied to the cooling coil to maintain a relativehumidity off the coil to below about 95% to about 99% RH.
 5. A method ofchilling inlet air to a gas turbine, comprising: a. a gas turbine thatincludes a gas turbine inlet; b. providing a system of circulatingliquid chilling water solution wherein the water solution contains waterplus an additive which is capable of reducing the freezing point ofwater; c. passing at least a portion of the liquid chilling watersolution through a first chiller and then a second chiller, the liquidchilling water solution passing through the first chiller being loweredto a first temperature; and the liquid chilling water solution passingthrough the second chiller being lowered to a second temperature whichis lower than the first; d. providing an inlet air chiller, comprising acooling coil through which the liquid chilling water solution passes,for lowering the temperature of inlet air being fed to the gas turbinecompressor through heat transfer between the liquid chilling watersolution passing through the cooling coil and the inlet air, and e.chilling the inlet air by directing the liquid chilling water solutionthrough the cooling coil of the inlet air chiller to make heat transfercontact between the liquid chilling water and the inlet air.
 6. Themethod of claim 5, wherein the chilling water solution comprises anadditive of sodium nitrate in an amount sufficient to decrease thefreezing temperature of the chilling water solution.
 7. The method ofclaim 5, wherein the chilling water solution comprises an additive ofpotassium formate in an amount sufficient to decrease the freezingtemperature of the chilling water solution.
 8. The method of claim 1,wherein the controlling the leaving air temperature off the cooling coilis accomplished by maintaining a leaving air temperature slightly abovethe dew point temperature of the ambient air.
 9. The method of claim 1,wherein the controlling the leaving air temperature off the cooling coilis based on an identified operating parameter associated with the gasturbine plant.
 10. The method of claim 9, wherein the operatingparameter is the dew point temperature of the ambient air.
 11. Themethod of claim 10, wherein the leaving air temperature is maintainedslightly above the operating parameter.
 12. The method of claim 9,wherein the operating parameter is the humidity of the ambient air. 13.The method of claim 9, wherein the operating parameter is the capacityrequirement for the gas turbine plant.
 14. The method of claim 1,wherein the inlet air temperature is adjusted by changing the flow rateof the liquid chilling water passing through the cooling coil.
 15. Themethod of claim 14, wherein the inlet air temperature is adjusted whenthe temperature difference between the liquid chilling water enteringthe cooling coil and the liquid chilling water leaving the cooling coilreaches a desired level.
 16. The method of claim 14, further comprising:providing a pump for circulating the liquid chilling water, wherein theflow rate of the liquid chilling water is reduced by lowering the speed(RPM) of the pump via a variable frequency drive on the pump.
 17. Themethod of claim 1, wherein the inlet air temperature is adjusted bylowering the temperature of the liquid chilling water when the inlet airtemperature increases above a setpoint.
 18. The method of claim 1,wherein the inlet air temperature is adjusted by providing a wet bulbtemperature sensor to monitor the ambient air wet bulb temperatureentering the cooling coil and lowering the temperature of the liquidchilling water when the ambient air wet bulb temperature increases. 19.A method for chilling inlet air to a gas turbine, comprising: providinga system of circulating water including a chilling system having a firstchiller, wherein water can pass through the first chiller, the waterpassing through the first chiller being lowered to a first temperature;providing an inlet air chiller for lowering the temperature of air beingfed to a gas turbine compressor through heat transfer between thecirculating water and the air; providing a storage tank which isoperably connected to the system of circulating water, the storage tankcontaining a column of water characterized by a top and a bottom; duringa charge cycle, removing water from the storage tank, passing at least aportion of the removed water through the chilling system to lower thetemperature of water passing through the chilling system and thenintroducing at least a portion of the removed water into the storagetank at a point proximate the bottom of the water column, wherein theaverage temperature of the water in the storage tank is lowered; duringa discharge cycle, chilling the air by removing water from the storagetank from a point proximate the bottom of the water column and thenpassing at least a portion of the removed water through the inlet airchiller to make heat transfer contact between that portion of theremoved water and the air, such that the temperature of the air islowered; and adjusting the temperature of the air based on an airtemperature setpoint that is varied by a control setpoint signal from acontrols system which adjusts the air temperature setpoint to maintainthe desired gas turbine output.
 20. A method for chilling inlet air to agas turbine, comprising: providing a system of circulating waterincluding a chilling system having a first chiller, wherein water canpass through the first chiller, the water passing through the firstchiller being lowered to a first temperature; providing an inlet airchiller for lowering the temperature of air being fed to a gas turbinecompressor through heat transfer between the circulating water and theair; providing a storage tank which is operably connected to the systemof circulating water, the storage tank containing a column of watercharacterized by a top and a bottom; during a charge cycle, removingwater from the storage tank, passing at least a portion of the removedwater through the chilling system to lower the temperature of waterpassing through the chilling system and then introducing at least aportion of the removed water into the storage tank at a point proximatethe bottom of the water column, wherein the average temperature of thewater in the storage tank is lowered; during a discharge cycle, chillingthe air by removing water from the storage tank from a point proximatethe bottom of the water column and then passing at least a portion ofthe removed water through the inlet air chiller to make heat transfercontact between that portion of the removed water and the air, such thatthe temperature of the air is lowered; selecting a desired airtemperature setpoint based on load requirements of the gas turbine; andadjusting the temperature of the air to the desired air temperaturesetpoint.
 21. The method of claim 20, wherein the temperature of the airis adjusted by changing the flow rate of the circulating water passingthrough the first chiller.
 22. The method of claim 20, wherein thetemperature of the air is adjusted in response to predetermined changesin ambient air wet bulb temperature.
 23. The method of claim 20, whereinthe temperature of the air is adjusted in response to predeterminedchanges in ambient air enthalpy.
 24. The method of claim 20, wherein thetemperature of the air is adjusted by varying the circulating water flowrate.
 25. The method of claim 20, wherein the temperature of the air isadjusted by varying the circulating water temperature.
 26. The method ofclaim 20, wherein the temperature of the air is adjusted by heating thecirculating water.
 27. The method of claim 26, wherein the circulatingwater is passed from the inlet air chiller to a heater and back to theinlet air chiller to increase the temperature of the air.
 28. The methodof claim 26, wherein the circulating water is heated to keep the massflow of the air within a desirable mass flow range.
 29. The method ofclaim 20, wherein the air temperature setpoint is a function of bothambient wet bulb temperature of the air and the temperature differencebetween the circulating water entering the inlet air chiller and thecirculating water leaving the inlet air chiller.
 30. The method of claim20, further comprising: providing chilling system controls and turbinecontrols, wherein the chilling system controls communicate with theturbine controls to control setpoints to optimize gas turbine output.31. The method of claim 20 wherein the first chiller is turned offduring peak periods to minimize the total amount of electricity requiredto power the chilling system.
 32. The method of claim 20, wherein theair temperature is adjusted by changing the flow rate of the circulatingwater passing through the inlet air chiller.
 33. The method of claim 20,wherein the air temperature is adjusted when the temperature differencebetween the circulating water entering the inlet air chiller and thecirculating water leaving the inlet air chiller reaches a desired level.34. A method for chilling inlet air to a gas turbine, comprising:providing a system of circulating water including a chilling systemhaving a first chiller, wherein water can pass through the firstchiller, the water passing through the first chiller being lowered to afirst temperature; providing an inlet air chiller for lowering thetemperature of air being fed to a gas turbine compressor through heattransfer between the circulating water and the air; providing a storagetank which is operably connected to the system of circulating water, thestorage tank containing a column of water characterized by a top and abottom; during a charge cycle, removing water from the storage tank,passing at least a portion of the removed water through the chillingsystem to lower the temperature of water passing through the chillingsystem and then introducing at least a portion of the removed water intothe storage tank at a point proximate the bottom of the water column,wherein the average temperature of the water in the storage tank islowered; during a discharge cycle, chilling the air by removing waterfrom the storage tank from a point proximate the bottom of the watercolumn and then passing at least a portion of the removed water throughthe inlet air chiller to make heat transfer contact between that portionof the removed water and the air, such that the temperature of the airis lowered; and maintaining the temperature of the air at a desired airtemperature setpoint based on load requirements of the gas turbine. 35.The method of claim 34, wherein the air temperature is maintained byreducing the flow rate of the circulating water passing through theinlet air chiller.
 36. The method of claim 34, wherein the airtemperature is maintained by reducing the flow rate of the circulatingwater passing through the first chiller.
 37. The method of claim 34,wherein the air temperature is maintained by adjusting the temperatureof the circulating water entering the inlet air chiller.
 38. The methodof claim 34, wherein the air temperature is maintained by heating thecirculating water.
 39. The method of claim 34, wherein the airtemperature setpoint is a function of both ambient wet bulb temperatureof the air and the temperature difference between the circulating waterentering the inlet air chiller and the circulating water leaving theinlet air chiller.
 40. The method of claim 34, wherein the airtemperature is maintained by utilizing a temperature sensor contactingthe air to monitor the temperature of the air.
 41. The method of claim34, wherein the air temperature is maintained by providing a wet bulbtemperature sensor to monitor the ambient air wet bulb temperatureentering the inlet air chiller.
 42. A method for chilling inlet air to agas turbine, comprising: providing a system of circulating waterincluding a chilling system having a first chiller, wherein water canpass through the first chiller, the water passing through the firstchiller being lowered to a first temperature; providing an inlet airchiller for lowering the temperature of air being fed to a gas turbinecompressor through heat transfer between the circulating water and theair; providing a storage tank which is operably connected to the systemof circulating water, the storage tank containing a column of watercharacterized by a top and a bottom; during a charge cycle, removingwater from the storage tank, passing at least a portion of the removedwater through the chilling system to lower the temperature of waterpassing through the chilling system and then introducing at least aportion of the removed water into the storage tank at a point proximatethe bottom of the water column, wherein the average temperature of thewater in the storage tank is lowered; during a discharge cycle, chillingthe air by removing water from the storage tank from a point proximatethe bottom of the water column and then passing at least a portion ofthe removed water through the inlet air chiller to make heat transfercontact between that portion of the removed water and the air, such thatthe temperature of the air is lowered; selecting a desired airtemperature setpoint for the air; and altering the air temperaturesetpoint of the gas turbine.
 43. The method of claim 42, wherein the airtemperature setpoint is altered based on changes in the loadrequirements of the gas turbine.
 44. The method of claim 42, wherein theair temperature setpoint is altered based on the time of day.
 45. Themethod of claim 42, wherein the air temperature setpoint is alteredbased on the ambient temperature.
 46. The method of claim 42, whereinthe air temperature setpoint is altered at off-design ambienttemperatures.
 47. The method of claim 46, wherein the air temperaturesetpoint is increased at reduced off-design ambient temperatures.
 48. Amethod for chilling inlet air to a gas turbine, comprising: providing asystem of circulating water including a chilling system having a firstchiller and a second chiller, the first and second chillers beingarranged in series, wherein water can pass through the first and secondchillers, the water passing through the first chiller being lowered to afirst temperature, the water passing through the second chiller beinglowered to a second temperature that is lower than the firsttemperature, thus providing a staged temperature drop; providing aninlet air chiller for lowering the temperature of the air being fed to agas turbine compressor through heat transfer between the circulatingwater and the air; providing a storage tank which is operably connectedto the system of circulating water, the storage tank containing waterand having a bottom; during a charge cycle, removing water from thestorage tank, passing at least a portion of the removed water throughthe chilling system to lower the temperature of water passing throughthe chilling system and then introducing at least a portion of theremoved water into the storage tank at a point proximate the bottom ofthe tank, wherein the average temperature of the water in the storagetank is lowered; and during a discharge cycle, chilling the air byremoving water from the storage tank from a point proximate the bottomof the tank and then passing at least a portion of the removed water tothe inlet air chiller to make heat transfer contact between that portionof the removed water and the air, such that the temperature of the airis lowered.
 49. The method of claim 48, further comprising adjusting theair temperature by changing the flow rate of the circulating waterpassing through the inlet air chiller.
 50. The method of claim 48,further comprising controlling leaving air temperature from the inletair chiller based on an identified operating parameter associated withthe gas turbine.
 51. The method of claim 50, wherein the operatingparameter is the capacity requirement for the gas turbine.
 52. A methodfor chilling inlet air to a gas turbine, comprising: providing a systemof circulating water including a chilling system having a first duplexchiller and a second duplex chiller, the first and second duplexchillers being arranged in series; providing an inlet air chiller forlowering the temperature of air being fed to a gas turbine compressorthrough heat transfer between the circulating water and the air; passingwater through the first and second duplex chillers, wherein the waterpassing through the first duplex chiller is lowered to a firsttemperature and then a second temperature that is lower than the firsttemperature, passing water through the second duplex chiller, whereinthe water temperature passing through the second duplex chiller islowered to a third temperature that is lower than the second temperatureand then a fourth temperature that is lower than the third temperature,thus providing a four stage temperature drop of the water; and passingat least a portion of the chilled water through the inlet air chillerresulting in heat transfer between the chilled water and the air, suchthat the temperature of the air is lowered.
 53. The method of claim 52,further comprising storing a portion of the chilled water from one ofthe chillers in a storage tank which is operably connected to the inletair chiller.
 54. The method of claim 52 wherein at least some of thecirculating chilling water is circulated through a thermal water storagetank during a charging cycle.
 55. A method for chilling inlet air to agas turbine, comprising: providing a system of circulating waterincluding a chilling system having a first chiller and a second chillerand a third chiller, the first and second and third chillers beingarranged in series; providing an inlet air chiller for lowering thetemperature of air being fed to a gas turbine compressor through heattransfer between the circulating water and the air; passing waterthrough the first, second and third chillers, wherein water passingthrough the first chiller is lowered to a first temperature, waterpassing through the second chiller is lowered to a second temperaturethat is lower than the first temperature, and water passing through thethird chiller is lowered to a third temperature that is lower than thesecond temperature, thus providing a staged temperature drop of thewater; and passing at least a portion of the chilled water through theinlet air chiller resulting in heat transfer between the chilled waterand the air, such that the temperature of the air is lowered.
 56. Amethod for chilling inlet air to a gas turbine, comprising: providing asystem of circulating water including a chilled water circuit having afirst duplex chiller and a second duplex chiller, the first and secondduplex chillers being arranged in series for circulating chilled waterin a first flow direction through the chilled water circuit; providing acirculating condenser water circuit that circulates cooling waterthrough the second duplex chiller and then through the first duplexchiller such that the condenser water circuit is counterflow to thechilled water circuit; providing an inlet air chiller for lowering thetemperature of air being fed to a gas turbine compressor through heattransfer between the circulating water and the air; passing chilledwater through the first duplex chiller, wherein the chilled waterpassing through the first duplex chiller is lowered from a firsttemperature to a second temperature that is lower than the firsttemperature; passing the chilled water from the first duplex chillerthrough the second duplex chiller, wherein the chilled water temperatureis lowered to a third temperature that is lower than the secondtemperature, thus providing a staged temperature drop of the chilledwater; passing at least a portion of the chilled water from the chilledwater circuit through the inlet air chiller resulting in heat transferbetween the chilled water and the air, such that the temperature of theair is lowered.
 57. A method for chilling inlet air to a gas turbine,comprising: providing a system of circulating water including a chillingsystem having a first chiller and a second chiller, the first and secondchillers being arranged in series; passing water through the firstchiller to lower the water temperature to a first temperature;thereafter, passing the water through the second chiller to lower thewater temperature to a second temperature that is lower than the firsttemperature, thus providing a staged temperature drop; providing aninlet air chiller for lowering the temperature of the air being fed to agas turbine compressor through heat transfer between the circulatingwater and the inlet air; providing a thermal water storage tank which isoperably connected to the system of circulating water, the thermal waterstorage tank containing chilling water; during a charge cycle, removingwater from the storage tank, passing at least a portion of the removedwater through the chilling system to lower the temperature of waterpassing through the chilling system and then introducing at least aportion of the removed water into the storage tank; and during adischarge cycle, chilling the air by removing chilling water from thethermal water storage tank and then passing at least a portion of theremoved water to the inlet air chiller resulting in heat transferbetween the chilled water and the air, such that the temperature of theair is lowered; and varying the flow of chilling water through the inletair chiller.
 58. The method of claim 57, wherein the staged temperaturedrop is maintained at least 20° F. or above.
 59. The method of claim 57,wherein the inlet air chiller is a specially circuited cooling coildesigned to provide a staged temperature rise of at least 20° F. orabove.